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<title>DSTO Scientific Publications</title>
<description>Scientific Publications from the Defence Science and Technology Organisation</description>
<link>http://www.dsto.defence.gov.au/publications/scientific.php</link>

<item>
	<guid isPermaLink="true">http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9947/</guid>
	<title>Scaling of cavity-flow wind-tunnel data</title>
	<description>
&lt;ul&gt;

&lt;li&gt;&lt;strong&gt;Author:&lt;/strong&gt; Jones, M.; Watmuff, J.&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Issue Date:&lt;/strong&gt; 10-Aug-2009 &lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Citation:&lt;/strong&gt; 13th Australian Aeronautical Conference, 9-12 March 2009, Melbourne, Australia&lt;/li&gt;

&lt;/ul&gt;

&lt;h2&gt;Abstract&lt;/h2&gt;&lt;p&gt;This paper examines the issues relevant to the interpretation and scaling of 
data obtained from wind tunnel experiments on flows over cavities. Data from twelve 
previously published experiments has been extracted and compared.  A 
characteristic of cavity flows is the aeroacoustic resonance that may occur 
under certain circumstances. Based on the comparison of the existing data 
sources, the important parameters affecting the observed resonant frequencies 
are identified and discussed. To provide a framework for the data analysis 
existing mathematical and physical models of cavity resonance are reviewed. 
Finally, some of the experimental issues surrounding measurements of 
aeroacoustic flows are discussed.&lt;/p&gt;
</description>
	<link>http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9947/</link>
</item>

<item>
	<guid isPermaLink="true">http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9927/</guid>
	<title>Emergent Naval Technology</title>
	<description>
&lt;ul&gt;

&lt;li&gt;&lt;strong&gt;Author:&lt;/strong&gt; Byrne, Duncan&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Issue Date:&lt;/strong&gt; 26-Jul-2009 &lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Citation:&lt;/strong&gt; Navy Futures Week 2009 at the Australian Command and Staff College Navy Single Service Future's Week, 9th June 2009.&lt;/li&gt;

&lt;/ul&gt;

&lt;h2&gt;Abstract&lt;/h2&gt;&lt;p&gt;Advances in technology will facilitate the development of a number of emerging concepts in the maritime environment that will increasingly be joint in nature. This presentation focuses on technologies and concepts that should be feasible in the 2020-2030 timeframe.&lt;/p&gt;
</description>
	<link>http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9927/</link>
</item>

<item>
	<guid isPermaLink="true">http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9949/</guid>
	<title>Testing Flight Paths for Collecting 3D LADAR Imagery of Inconspicuous Targets</title>
	<description>
&lt;ul&gt;

&lt;li&gt;&lt;strong&gt;Author:&lt;/strong&gt; Mewett, David; Graham, Mark; Davies, Adam&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Issue Date:&lt;/strong&gt; Jul-2009 &lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Citation:&lt;/strong&gt; Mewett, D.T., M.D. Graham and A.H. Davies (2009).  Testing flight paths for collecting 3D LADAR imagery of inconspicuous targets. In Anderssen, R.S., R.D. Braddock and L.T.H. Newham (eds) 18th World IMACS Congress and MODSIM09 International Congress on Modelling and Simulation. Modelling and Simulation Society of Australia and New Zealand and International Association for Mathematics and Computers in Simulation, July 2009, pp. 1636-1642. ISBN: 978-0-9758400-7-8. http://www.mssanz.org.au/modsim09/E1/mewett.pdf&lt;/li&gt;

&lt;/ul&gt;

&lt;h2&gt;Abstract&lt;/h2&gt;&lt;p&gt;A pilot study was performed to examine flight paths for an airborne foliage-penetrating Laser
Detection and Ranging (LADAR) three-dimensional (3D) imaging system. Such systems form 3D images
based on time-of-flight of laser photons, some of which pass through gaps in foliage or other partial
obscurants such as camouflage nets. Hence the 3D image will contain partial information about any objects
behind or underneath such obscurants. The obscurant can be removed from the image by only keeping points
within some appropriate range, leaving a partial image of the hidden objects which may include targets of
interest. An improved overall image can be formed by combining images taken from several different
viewpoints, using knowledge of the LADAR sensors location at each viewpoint. In this study, we compared
the overall 3D images obtained from an airborne LADAR system during different flight paths.
The scene for each flight path consisted of a four-wheel-drive vehicle placed in a section of a eucalypt forest.
Models for the vehicle and the individual trees were created in the 3D modelling software Maya, and
exported as point clouds to be used in the general-purpose analysis software MATLAB. The overall forest
scene was then assembled from the individual trees. The amount of light penetrating the foliage was
determined at three different locations within the scene. On average, results were found to roughly agree with
the prediction that light penetration scales with the sine of the angle from horizontal.
Formation of LADAR images was modelled by determining the set of points in the scene that had a direct
line-of-sight to the airborne sensor. This low-fidelity approach was taken because the aim of the study was to
investigate ways of tasking the sensor system, rather than using the model as part of a hardware design
process or a testbed for data processing algorithms. Since there is already a random effect due to line-of-sight
through the forest canopy, it was decided that further random effects leading to false returns or missed returns
would unnecessarily complicate the comparison between results from different flight paths.
The flight paths in this study were intended to keep the sensor footprint directed at a known or assumed
target area on the ground. One type of path was an arc centred at this location, with the sensor constantly
directed sideways at an appropriate elevation. The other type of path went straight past the target area, with
the sensor needing to be constantly redirected. Different scan spacings along the path were also investigated.
It was assumed that the unobscured view from each flight path would be sufficient for the surveillance or
reconnaissance task. So for each flight path, the Hausdorff distance was calculated as a measure of the
difference between the 3D image of the target taken through the foliage and the corresponding unobscured
image from the same flight path. No significant difference was found between results for the straight and arc
paths, but the 3D images were closest to the unobscured views for the smallest scan spacing.&lt;/p&gt;
</description>
	<link>http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9949/</link>
</item>

<item>
	<guid isPermaLink="true">http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9995/</guid>
	<title>Benchmark Testing of Naval Threat Countermeasure Simulation (NTCS) Development from Version 2.4c to 3.2.</title>
	<description>
&lt;ul&gt;

&lt;li&gt;&lt;strong&gt;Report Number:&lt;/strong&gt; DSTO-TR-2315&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Author:&lt;/strong&gt; Smith, S.E.&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Issue Date:&lt;/strong&gt; 2009-07&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;AR Number:&lt;/strong&gt; AR-014-578&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Classification:&lt;/strong&gt; Unclassified&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Report Type:&lt;/strong&gt; Technical Report&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Division:&lt;/strong&gt; Maritime Platforms Division (MPD)&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Release Authority:&lt;/strong&gt; Chief, Maritime Platforms Division&lt;/li&gt;

&lt;/ul&gt;

&lt;h2&gt;Abstract&lt;/h2&gt;&lt;p&gt;The Naval Threat Countermeasure Simulator (NTCS) is a commercial code accepted as the NATO standard for ship Infrared (IR) signature modelling. This code has undergone extensive development, in conjunction with measurement trials, since 1997. A set of benchmark test cases was developed to track the development of NTCS since 1997 paying particular attention to the effect on the computed IR signature of a test target. In this report, the results from these benchmark tests are presented for NTCS versions from 2.4c to 3.2. It will be shown that improvements to the NTCS code from version to version result in significant changes in computed IR signatures. In addition to code changes, other parameters such as choice of environmental data generation software (e.g. LOWTRAN/MODTRAN) and choice of solar scattering flag also influence the computed IR signature. Timing information was also assessed as
part of this study and reveals increases in run-time requirements as NTCS has evolved. In light of these results, caution should be exercised when comparing results from different versions of NTCS. It is also recommended that details of the NTCS version and parameters used are specified when presenting NTCS results.&lt;/p&gt;

&lt;h2&gt;Executive Summary&lt;/h2&gt;&lt;p&gt;The Naval Threat Countermeasure Simulator (NTCS) is a commercial code accepted as the NATO standard for ship infrared (IR) signature modelling. This code has undergone extensive development, in conjunction with measurement trials, since 1997. A set of benchmark test cases was developed to track the development of NTCS since 1997 paying particular attention to the effect on the computed IR signature of a test target. In this report, the results from these benchmark tests are presented for NTCS versions from 2.4c to 3.2. In addition to the changes resulting from different version, two other parameters within NTCS were also investigated. The first is the choice of environmental data generation software (e.g. LOWTRAN/MODTRAN) and the second is the choice of the solar scattering flag. These were included since they were changed or added to NTCS within the series of NTCS from 2.4c to 3.2.
Improvements to the NTCS code from version to version result in significant changes in computed IR signatures. In addition to code changes, the parameters such as choice of environmental data generation software and choice of solar scattering flag also influence the computed IR signature. Timing information was also assessed during this study and reveals that the run-time requirements for NTCS have increased during the evolution of NTCS. It is recommended that caution is exercised when comparing results from different versions of NTCS. It is also recommended that details of the NTCS version and parameters used are specified when presenting NTCS results. Accurate comparisons of computed IR contrast signature data for different naval platforms can only be made reliably when the same NTCS version is used and the same background, environmental data generation software and solar scattering flag are selected.&lt;/p&gt;
</description>
	<link>http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9995/</link>
</item>

<item>
	<guid isPermaLink="true">http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9996/</guid>
	<title>Survey of Knowledge Representation and Reasoning Systems.</title>
	<description>
&lt;ul&gt;

&lt;li&gt;&lt;strong&gt;Report Number:&lt;/strong&gt; DSTO-TR-2324&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Author:&lt;/strong&gt; Trentelman, K.&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Issue Date:&lt;/strong&gt; 2009-07&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;AR Number:&lt;/strong&gt; AR-014-588&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Classification:&lt;/strong&gt; Unclassified&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Report Type:&lt;/strong&gt; Technical Report&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Division:&lt;/strong&gt; Command, Control, Communication and Intelligence Division (C3ID)&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Release Authority:&lt;/strong&gt; Chief, Command, Control, Communication and Intelligence Division&lt;/li&gt;

&lt;/ul&gt;

&lt;h2&gt;Abstract&lt;/h2&gt;&lt;p&gt;As part of the information fusion task we wish to automatically fuse information
derived from the text extraction process with data from a structured
knowledge base. This process will involve resolving, aggregating, integrating
and abstracting information - via the methodologies of Knowledge Representation
and Reasoning - into a single comprehensive description of an individual
or event. This report surveys the key principles underlying research in the
field of Knowledge Representation and Reasoning. It represents an initial step
in deciding upon a Knowledge Representation and Reasoning system for our
information fusion task.&lt;/p&gt;

&lt;h2&gt;Executive Summary&lt;/h2&gt;&lt;p&gt;As part of the information fusion task we wish to automatically fuse information derived
from the text extraction process with data from a structured knowledge base. This process
will involve resolving, aggregating, integrating and abstracting information - via the
methodologies of Knowledge Representation and Reasoning - into a single comprehensive
description of an individual or event. This report surveys the key principles underlying
research in the field of Knowledge Representation and Reasoning. It represents an
initial step in deciding upon a Knowledge Representation and Reasoning system for our
information fusion task.
We find that although first-order logic is a highly expressive knowledge representation
language, a major drawback of the logic as a Knowledge Representation and Reasoning
system for our information fusion task is its undecidability. Moreover, most first-order automated
theorem provers are not designed for large knowledge-based applications. Modal
logics are gradually receiving more attention by the Artificial Intelligence community,
but research in modal logics for knowledge representation still has a long way to go. A
production rule (expert) system is viable as a Knowledge Representation and Reasoning
system, but these systems are optimally suited for small, specific domains. To build an
intelligence expert system we would require expert knowledge in pretty much everything.
Frame systems are limited in their expressiveness, and moreover - in regards to knowledge
representation - have been superceded by description logics. Semantic networks are excellent
for taxonomies, but are not particularly suitable for our information fusion task. On
a more positive note, description logics are currently very popular and are actively being
researched. They are (in the most part) decidable and their open-world semantics would
allow us to represent incomplete information. A further advantage is the availability of
Semantic Web technologies. Description logics are still limited however; for our task, wed
need to look at very expressive logics which might lose us decidability.&lt;/p&gt;
</description>
	<link>http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9996/</link>
</item>

<item>
	<guid isPermaLink="true">http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9997/</guid>
	<title>Giselle: A Mutually Orthogonal Triple Twin-loop Ground-symmetrical Broadband Receiving Antenna for the HF Band.</title>
	<description>
&lt;ul&gt;

&lt;li&gt;&lt;strong&gt;Report Number:&lt;/strong&gt; DSTO-TR-2321&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Author:&lt;/strong&gt; Martinsen, W.&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Issue Date:&lt;/strong&gt; 2009-07&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;AR Number:&lt;/strong&gt; AR-014-584&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Classification:&lt;/strong&gt; Unclassified&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Report Type:&lt;/strong&gt; Technical Report&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Division:&lt;/strong&gt; Command, Control, Communication and Intelligence Division (C3ID)&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Release Authority:&lt;/strong&gt; Chief, Command, Control, Communication and Intelligence Division&lt;/li&gt;

&lt;/ul&gt;

&lt;h2&gt;Abstract&lt;/h2&gt;&lt;p&gt;This report describes development of a tri-axial mutually orthogonal broadband twin-loop
receiving antenna for the HF band. The three twin-loops have been arranged so that they exhibit
the same distributed parameters between themselves and ground. The upper frequency limit of
the antenna is discussed and a method for extending the low frequency cut-off is presented. The
antenna noise factor is calculated from measured data.&lt;/p&gt;

&lt;h2&gt;Executive Summary&lt;/h2&gt;&lt;p&gt;Traditional mutually orthogonal tri-axial loop antennas have distributed parameters to the
ground that are not consistent between the three loops. This non-symmetrical
characteristic adds complexity to the analysis of signals received from each of the loops.
Also, the distributed inductance (L) and capacitance (C) of each loop form a resonant
circuit limiting the loops usefulness for broadband work.
The tri-axial twin-loop antenna design presented in this report has the same distributed
parameters to ground on all three loops (ground-symmetrical) easing the analysis burden
on the received data. The final version of the antenna presented can cover the complete HF
band and is ideal for studying the polarisation of received signals with the view of
mitigating HF polarisation fading.
The inherent noise produced by the Giselle antenna is less than the expected man-made
noise for a quiet rural site; therefore the Giselle antenna can also be used as a compact triaxial
polarisation diversity surveillance antenna for the whole of the HF band. It is capable
of discriminating between locally transmitted ground wave signals and those transmitted
at some distance and received via sky-wave by monitoring for any signs of rotation in the
received signals polarisation.&lt;/p&gt;
</description>
	<link>http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9997/</link>
</item>

<item>
	<guid isPermaLink="true">http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9998/</guid>
	<title>Synthetic Electronic Imaging System.</title>
	<description>
&lt;ul&gt;

&lt;li&gt;&lt;strong&gt;Report Number:&lt;/strong&gt; DSTO-TN-0903&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Author:&lt;/strong&gt; Ide, K.M.; Jarvis, B.J.; Lucas, M.A.&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Issue Date:&lt;/strong&gt; 2009-07&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;AR Number:&lt;/strong&gt; AR-014-574&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Classification:&lt;/strong&gt; Unclassified&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Report Type:&lt;/strong&gt; Technical Note&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Division:&lt;/strong&gt; Weapon Systems Division (WSD)&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Release Authority:&lt;/strong&gt; Chief, Weapons Systems Division&lt;/li&gt;

&lt;/ul&gt;

&lt;h2&gt;Abstract&lt;/h2&gt;&lt;p&gt;The Synthetic Electronic Imaging System employs electronic components to combine multiple images from a plurality of cameras which are processed with inertial data from the vehicle on which the system is mounted to yield stabilised video images without resorting to complicated optics or a stabilised platform. It was devised as an alternative to stabilised ball turrets fitted with electro-optic and infrared cameras. Intended as an imaging system for Unmanned Aerial Vehicles (UAV), it may be employed in any manned or Unmanned System (UMS) where situation awareness is aided by the use of an imaging system. This report describes the development of the Synthetic Electronic Imaging System and assembly of a simple concept demonstrator in 2005.&lt;/p&gt;

&lt;h2&gt;Executive Summary&lt;/h2&gt;&lt;p&gt;Conventional ball turret imaging systems are mechanically complex requiring continued calibration and maintenance. Hence, their purchase and support involves significant costs. The dimensions and weight of a ball turret demand an airframe with significant payload capacity. These restrictions led the authors to develop the Synthetic Electronic Imaging System. It is a highly capable alternative but without the complexity, cost and support necessary for a comparable ball turret imaging system. 
The Synthetic Electronic Imaging System employs electronic components to combine multiple images from a plurality of cameras which are processed with inertial data from the vehicle on which the system is mounted to yield stabilised video images without resorting to complicated optics or a stabilised platform. A full field of view wide angle composite image is displayed on one monitor with a box overlay representing the region of interest. A second monitor shows a telephoto image within the designated region of interest. As the operator moves the region of interest, images in the second display are updated in real-time. The two complementary video streams provide an excellent aid to situation awareness and analysis. 
The two video channels are transmitted to the Ground Control Station as television images requiring very low bandwidth. Operators can time-slip the video images by using Digital Video Recorder software controls for review and analysis. Frames that merit further analysis or examination can be downloaded from the remote vehicle as a series of still images with the maximum resolution of the sensor. 
Intended as an imaging system for Unmanned Aerial Vehicles, it may be employed in any manned or Unmanned System where situation awareness is aided by the use of an imaging system. This report describes the development of the Synthetic Electronic Imaging System and assembly of a simple concept demonstrator in 2005.&lt;/p&gt;
</description>
	<link>http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9998/</link>
</item>

<item>
	<guid isPermaLink="true">http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9992/</guid>
	<title>Thermodynamically Consistent Decoupled Shear-Volumetric Strain Model and CTH Implementation.</title>
	<description>
&lt;ul&gt;

&lt;li&gt;&lt;strong&gt;Report Number:&lt;/strong&gt; DSTO-TR-2299&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Author:&lt;/strong&gt; Resnyansky, A.D.&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Issue Date:&lt;/strong&gt; 2009-06&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;AR Number:&lt;/strong&gt; AR-014-552&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Classification:&lt;/strong&gt; Unclassified&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Report Type:&lt;/strong&gt; Technical Report&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Division:&lt;/strong&gt; Weapon Systems Division (WSD)&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Release Authority:&lt;/strong&gt; Chief, Weapons Systems Division&lt;/li&gt;

&lt;/ul&gt;

&lt;h2&gt;Abstract&lt;/h2&gt;&lt;p&gt;Many hydrocodes, such as LS-DYNA and CTH, require the decoupling of the shear from volumetric response in a material model used. A constitutive model is formulated, which decouples the responses of a rate sensitive material. Basis of the model is a general Maxwell-type viscoelastic model, which, however, is not originally decoupled and, thus, not suitable for implementation in the hydrocodes. The formulation provides the thermodynamic consistency for the case of small deviatoric elastic deformations and unrestricted volumetric response. A schematic of implementation in CTH is briefly described. Numerical illustrations demonstrate agreement of the CTH calculations with calculations available in the literature.&lt;/p&gt;

&lt;h2&gt;Executive Summary&lt;/h2&gt;&lt;p&gt;The development of advanced weaponry demands science and industry pay attention to novel energetic materials and materials with enhanced protective properties, including composite materials, porous and multi-phase mitigants, advanced materials manufactured with nanotechnology, etc. The response of these materials needs to be predicted and this raises new challenges for the area of computer modelling of the material response to extreme pressure and temperature. Advanced shock physics codes are a solid basis for modelling efforts. Among them hydrocodes are the most relevant to the level of loads and temperatures because they are able to deal both with the material behaviour in conditions of hydrodynamic flow and with the elastic-plastic deformation at moderate loads when the material strength is important. Hydrodynamic (strength negligible) flows due to extreme loads are typical for materials subject to the hyper-velocity impact by shaped charge jets and for materials in direct contact with detonating energetic materials. The effect of these conditions on enhanced materials requires consideration of multi-phase behaviour with phase transitions, however, such models are yet to be developed. The elastic-plastic (strength relevant) deformations prevail in materials at the load levels typical of high-velocity fragmentation impact or of blast effects from charges in a certain proximity to the target. The elastic-plastic response under these conditions is of the constitutive type, i.e., the materials manifest rate sensitivity and require advanced modelling approaches. In summary, the development and use of advanced models in commercially available hydrocodes is a great challenge. 
The modelling capability in DSTO is supported by several hydrocodes. The LS-DYNA3D hydrocode (originally a Lagrangian code) has been employed for a number of years in DSTO. It has proved its efficiency for modelling the weapon and terminal effects in problems involving moderate deformations and requiring a good resolution of contact material interfaces. A user-defined material model is relatively simple to incorporate within the DYNA interface though no well-documented implementation procedures are established. A number of material models have been implemented in this code in DSTO exploring the constitutive model capabilities for: i)conventional materials subject to high-velocity fragment impact [1] and materials involved in the shaped charge jet formation, when studying the weapon effects of the two-stage follow-through grenade weapon [2], ii)composite materials subject to ballistic impact for the Army Reconnaissance Helicopter project [3],iii)concretes subject to hyper-velocity impact, when studying the target effects against the multi-stage weapon threats [2, 4], and iv)materials manifesting multi-phase features, when simulating the underwater explosion in a Navy project [5].  However, for the problems such as counter-IED (Improvised Explosive Devices) dealing with large deformations, intensive flows and high multi-phase/multi-material mixing a Eulerian code is more suitable. Therefore, the present work is attempting to gather the implementation experience for the CTH hydrocode developed by Sandia National Laboratories in the US. Implementation procedures for the code are quite well documented. The implementation difficulties are mainly associated with the necessity for the user to intervene in a number of entry points of the code, the number of which and the places of entry depend on the nature of the model to be incorporated. Due to the release features of the code not all necessary points of entry may be easily accessible, this is another challenge for the user. 
The present work adapts a rate sensitive strength model for conventional materials, which has been published earlier in the literature, to a form decoupling the shear and volumetric responses. The present formulation is in agreement with the CTH implementation requirements and it preserves the thermodynamic consistency of the model. In addition, this formulation suggests a general thermodynamically consistent way of decoupling between the shear and volumetric responses of a material, which might be useful for the development of advanced strength models requiring this decoupling. The model along with its implementation is tested with a number of impact and shaped charge problems. The CTH calculations are compared with numerical solutions and experiments available in the literature and a good agreement is observed. Thus, the present work establishes the model implementation capability in DSTO for the CTH hydrocode.&lt;/p&gt;
</description>
	<link>http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9992/</link>
</item>

<item>
	<guid isPermaLink="true">http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9993/</guid>
	<title>Acoustic Electric Feedthrough Demonstrator Mk-I.</title>
	<description>
&lt;ul&gt;

&lt;li&gt;&lt;strong&gt;Report Number:&lt;/strong&gt; DSTO-TR-2296&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Author:&lt;/strong&gt; Moss, S.; Konak, M.; Phoumsavanh, C.; Tsoi, K.; Powlesland, I.&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Issue Date:&lt;/strong&gt; 2009-06&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;AR Number:&lt;/strong&gt; AR-014-549&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Classification:&lt;/strong&gt; Unclassified&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Report Type:&lt;/strong&gt; Technical Report&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Division:&lt;/strong&gt; Air Vehicles Division (AVD)&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Release Authority:&lt;/strong&gt; Chief, Air Vehicles Division&lt;/li&gt;

&lt;/ul&gt;

&lt;h2&gt;Abstract&lt;/h2&gt;&lt;p&gt;This report outlines the development and characterization of the DSTO Acoustic Electric Feedthrough (AEF) Laboratory Demonstrator Mk-I, which passes power ultrasonically through a 5 mm thick aluminium plate. The AEF approach is being explored as a potential means of wirelessly powering in situ structural health monitoring systems embedded within aircraft and other high value assets. The demonstrator's assembly and subsequent characterisation is discussed, and compared with performance predictions made using numerical modelling. Improvements are suggested which will be implemented in the proposed AEF Demonstrator Mk-II, a system capable of passing both power and communications ultrasonically through a metal plate.&lt;/p&gt;

&lt;h2&gt;Executive Summary&lt;/h2&gt;&lt;p&gt;This report has examined the modelling, characterization and manufacture of an Acoustic Electric Feedthrough (AEF) Laboratory Demonstrator Mk-I with the aim of developing a system capable of passing power and communications through the aluminium skin of an aircraft using ultrasound. An AEF arrangement operates via two piezoelectric elements, located collinearly on opposite sides of a metal plate. One piezoelectric element is excited at its thickness mode anti-resonant frequency which then generates ultrasound which passes through the metal plate, and is received by a second element located on the opposite side of the plate. A numerical model of the AEF demonstrator was developed and used to characterize the behaviour of the system; predictions from the numerical model were confirmed by experiment. Real power transfer efficiency was found to be 30% for the demonstrator. In particular the AEF power loss mechanisms were explored, and the major losses were heat generation due to viscous loss in the piezoelectric elements. An AEF Laboratory Demonstrator Mk-II that can transmit power (at the measured power transfer efficiency) and two-way communications is proposed.&lt;/p&gt;
</description>
	<link>http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9993/</link>
</item>

<item>
	<guid isPermaLink="true">http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9903/</guid>
	<title>Australian Defence Force Nutritional Requirements in the 21st Century (Version 1).</title>
	<description>
&lt;ul&gt;

&lt;li&gt;&lt;strong&gt;Report Number:&lt;/strong&gt; DSTO-GD-0578&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Author:&lt;/strong&gt; Forbes-Ewan, C.&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Issue Date:&lt;/strong&gt; 2009-05&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;AR Number:&lt;/strong&gt; AR-014-525&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Classification:&lt;/strong&gt; Unclassified&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Report Type:&lt;/strong&gt; General Document&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Division:&lt;/strong&gt; Human Protection and Performance Division (HPPD)&lt;/li&gt;

&lt;li&gt;&lt;strong&gt;Release Authority:&lt;/strong&gt; Chief, Human Protection and Performance Division&lt;/li&gt;

&lt;/ul&gt;

&lt;h2&gt;Abstract&lt;/h2&gt;&lt;p&gt;This report addresses the determinants of military nutritional requirementsthat is, the relevant
variables that determine the types and quantities of foods necessary to support ADF training and
operationsand the current state of knowledge about nutritional requirements. It also includes
recommendations on nutritional standards for ADF rationing systems, and suggests areas of
research that will help fill the gaps in our knowledge. Nutritional standards are recommended for
fresh (i.e. in-barracks or garrison) feeding and for combat ration packs. These standards are based
largely on the Nutrient Reference Values recommended by the National Health and Medical
Research Council for Australia and New Zealand, but include specific Military Nutrient
Reference Values for certain key nutrients.&lt;/p&gt;

&lt;h2&gt;Executive Summary&lt;/h2&gt;&lt;p&gt;This report addresses the determinants of military nutritional requirementsthat is, the
relevant variables that determine the types and quantities of foods necessary to support
ADF training and operations. It also examines the current state of knowledge about
nutritional requirements, includes recommendations on nutritional standards for ADF
rationing systems, and suggests areas of research that will help fill the gaps in our
knowledge.
This is the second revision (i.e. the third iteration) of Australian Defence Force Nutritional
Requirements in the 21st Century. However, although the two earlier documents were
internal reports, i.e. they were not published in the DSTO Report Series, they were used
by the Defence Materiel Organisation (DMO) to set standards for ADF combat ration
packs (CRP) and by DSTO to assess the nutritional adequacy of CRP and of fresh-feeding
systems.
The recent publication by the National Health and Medical Research Council (NHMRC,
2006) of Nutrient Reference Values for Australia and New Zealand provided an incentive
and an opportunity to revise and update this report. It is intended to be a living
documenti.e. it will be available only in electronic form and not in hard copyso it can
be updated whenever new information becomes available.
The 2009 Defence White Paper (Department of Defence, 2009) imposes on the ADF a need
for self-reliance, a high level of mobility, and an ability to operate in all terrains, climatic
conditions and social situations. Therefore, there is a need for rationing systems
(particularly ration packs) that will sustain troops during short-term, high-intensity
operations (e.g. up to 72 hours) and also a need for rationing systems that will support
long-term, low-intensity operations (lasting many weeks). In each case, operations could
be conducted in the heat, cold and/or at altitude, in rainforest, desert or temperate
regions.
Physical activity levels and gender are the two major determinants of nutritional
requirements of ADF members, with age, stature, climate, altitude, terrain, and individual
variation playing relatively minor roles. Each of these determinants exerts its effects
predominantly via an influence on energy expenditure. Females have approximately 70
75% of the energy requirement that males have for the same activity. The only substantial
purely gender-related difference in nutritional requirements is a greater need for iron by
female ADF members.
However, the unique requirements of adolescent ADF members should be taken into
account in messes where adolescents constitute a substantial proportion of the ADF population being rationed. Adolescent ADF members have a slightly greater need than
adults for energy for growth, and generally also for physical activity. Adolescents also
have a significantly greater need than adults of the same gender for some micronutrients,
particularly calcium (males and females), phosphorus (males and females) and iron (males
only).
The nutritional requirements discussed for ADF members in this document will not
necessarily apply to each individual. Although the ADF population is relatively
homogeneous, there will always be some variation between individuals. This variation
comes from two main sourcesdifferent body size and composition, and individual
genetic variation in metabolism. However, largely because requirements will vary
normally (in the statistical sense) about the mean, it is considered appropriate to base
nutritional standards on the nutritional requirements of average male and average female
members of the ADF.
The extent of over-nutrition (i.e. excess body fat levels) in the ADF needs to be
investigated. The Australian Defence Health Status Report (published in 2000) found that
57% of ADF members were above the healthy weight range. Recommendations are made
in the present report on how improvements may be made to monitoring and reporting of
body fat levels and determining risk of ill-health through the addition of a simple
measurementwaist circumferenceto existing regular medical examinations.
It appears to be a near-universal finding that troops under-eat on operations when
rationing is by CRP. When nutrient intake is less than ideal, the nutritional status of a
subject prior to the period of low nutrient intake itself becomes a determinant of
subsequent nutritional status. There is evidence from the military scientific literature (both
Australian and overseas) that young service people are entering military service with suboptimal
nutritional status. The potential for this to impact adversely on health and
performance can only be overcome by improvements in nutritional quality of diet during
service. This implies a strong need for both availability of highly-nutritious food and
guidance to ADF members on appropriate food selections to maximise nutritional status.
DSTO has conducted studies to determine the energy expenditure (and therefore
nutritional requirements) of (predominantly male) ADF members across a wide range of
land-based, and a smaller range of sea-based military activities. These results are
summarised in Tables 1 and 2 of the present report. Knowledge gaps can be filled by
conducting research on ADF groups not previously studied. There is also scope for
resuming the development of an expert system that will allow commanders to determine
the food and water needed to sustain troops in particular operational situations.
It is concluded that for the purposes of setting nutritional standards, the ADF can be
divided into four population groupsadult males, adult females, adolescent males and
adolescent females. Further, adult male ADF occupations can be conveniently assigned to
five distinct categories of energy expenditure, while four categories apply to occupations
involving adult females and adolescents. The highest category (Category 5) is believed to
be a special case, applying largely to males attempting selection to the Special Air Service
Regiment. Therefore, only categories 14 are regarded as being of practical significance to
the vast majority of ADF rationing. However, further studies on the energy expenditures
associated with SF training and operations are needed to confirm or alter this belief. Also,
it is suggested that during a period of re-feeding following sustained under-consumption
(e.g. when troops have been fed with combat ration packs for more than two weeks while
engaging in very vigorous physical activities), Category 5 entitlements are appropriate for
the period of re-feeding.
Although there is a reasonable correlation between the defined categories of ADF activity
levels and those of the NHMRC (2006), they do not correspond exactly. Consequently, it is
recommended that DSTO attempt to add a category of energy expenditure (perhaps
designated extreme activity) to the six existing NHMRC physical activity levels.
Nutritional quality of the diet of ADF members is critical in ensuring that optimal
performance can be maintained as long as possible. This quality is in terms of
macronutrients (protein, fat and carbohydrate), micronutrients (vitamins, minerals and
trace elements) and dietary fibre.
Carbohydrate is considered to be the most important macronutrient for vigorous physical
activity, with fat being of value mainly for acceptability. The important role played by
protein in recovery from vigorous physical activity has been recognised only relatively
recently. It is recommended that the standard for protein be set at 1520% of total energy
for situations involving light physical activity (Category 1), with the range of percentage
contributions decreasing linearly as energy expenditure increases (from 1419% for
Category 2 to 1114% for Category 5). Conversely, the percentage of energy derived from
carbohydrate should increase linearly with increasing physical activity from a range of
5055% (Category 1) to 5863% (Category 5), at the expense of fat (decreasing linearly from
2735% (Category 1) to 2331% (Category 5). The recommended ratios of protein to fat to
carbohydrate (P:F:C ratios) are shown in Table 4.
As indicated in a footnote to Table 4, the only situation in which it is recommended that
carbohydrate should provide more than 63% of energy is when operations are conducted
at high altitudehere it is recommended that the P:F:C ratio should be approximately
15:20:65 respectively.
There is preliminary evidence that not only the quantity, but also the quality of
carbohydrate may impact on both performance and health. Further research is warranted
on the potential to enhance nutritional status by varying the glycaemic index and
increasing resistant starch in rations (particularly in combat ration packs).
There is also scope for conducting research on the impact of combining protein with
carbohydrate to enhance recovery from vigorous physical activity.
The previous two iterations of this report included Recommended Military Dietary Intakes
(RMDIs) for all nutrients that had been assigned Recommended Dietary Intakes (RDIs) in
1991 by the NHMRC. The RMDIs corresponded very closely to the RDIs.
In 2006 the NHMRC published Nutrient Reference Values (NRVs) to apply to the
population of Australia and New Zealand. These differ, often substantially, from the 1991
recommendations. It is recommended that the RDIs (or Adequate Intake if an RDI has not
been established) of the NHMRC (2006) be adopted as Military Recommended Dietary
Intakes (MRDIs) for all nutrients other than thiamin, riboflavin, niacin, vitamin B6, protein
and sodium, and also for total energy. The reasons for these exceptions are detailed in the
body of this report. It is also recommended that MRDIs be defined for carbohydrate, even
though NRVs were not published by the NHMRC for carbohydrate. It is recommended
that military-specific Estimated Average Requirements (MEAR) be calculated for the Bgroup
vitamins thiamin, riboflavin, niacin and vitamin B6 as 70% of the respective MRDIs.
Finally, it is argued that nutritional standards should take into account age (adult versus
adolescent), gender and activity level. Table 5 shows the MRDIs for adult males for five
categories of physical activity; Tables 68 show the MRDIs for the adult females, adolescent
males and adolescent females of the ADF for four categories of activity.
Nutritional standards are recommended for general purpose (i.e. not mission-specific)
CRP. These are based on Category 3 requirements for energy (~16 MJ), protein and
carbohydrate for adult males and the MRDI that constitutes the worst case situation for
each micronutrient (i.e. the sub-group that has the greatest requirement for each specific
micronutrient) for ADF members working at Category 3 That is, the nutritional
requirements of practically all ADF members working at Category 3 will be met by the
basic ration pack if it is eaten in its entirety. Table 9 details the recommended nutritional
criteria for general purpose ration packs.
Further, it is recommended that fortification to three times the MRDI should occur for four
key vitaminsthiamin, riboflavin, vitamin B6 and vitamin Cto counteract storage losses
and the discarding of ration pack items. It is also recommended that more research be
conducted into vitamin stability during storage of ration packs, and on how bioavailability
of micronutrients from combat ration packs affects nutritional status of ADF members.
It is recommended that a small range of mission-specific ration packs be developed; that
consideration be given to adopting a modular, just-in-time process for procuring, packing
and distributing CRP; and that investigation be conducted into the need for, and most
appropriate form of a group-feeding pack.
Recommendations are provided on how entitlements to fresh rations should be
determined.
Tables 58 show the MRDIs that apply for homogeneous groups of ADF members (i.e. all
members are of the same gender and age groupadult or adolescent).
For a mixed ADF population (a mixture of genders and age groups) the entitlements to
energy and macronutrients for fresh feeding should be based on the number to be fed and
the MRDIs that apply to the worst case situation (i.e. the sub-group that has the greatest
requirement for each specific nutrient). Table 10a shows these recommended entitlements.
Appendix B provides an example of how the entitlements to total energy can be
determined for a mixed ADF population to be fed freshly-cooked food at a mess.
In designing ration scales for fresh feeding, it is recommended that a basic scale be devised
based on the MRDIs for energy, protein and carbohydrate for adolescent males working at
Category 1. For the remaining nutrients, the MRDI that applies to Category 4 physical work
output for the population sub-group that constitutes the worst case situation should
apply. Table 10c shows the recommended nutritional basis of the basic fresh-feeding scale.
Allowance should also be made for inevitable food discarding. It is suggested that this
allowance be 15%i.e. food availability should be 15% above the estimated requirement.
To feed troops working above Category 1, it is recommended that between-meal snacks be
devised in modular form, with each module providing 12 MJ.
Dietary modelling should be conducted to determine the ability of real world diets based
on these entitlements to meet the MEARs of ADF members. Table 10b shows the
nutritional criteria for this dietary modelling for mixed population groups of ADF
members. Table 10d shows the nutritional criteria for modelling the adequacy of the basic
ration scale (Category 1, mixed population).
In assessing the nutritional adequacy of intake of ADF groups it is also the MEARs that
apply. Table 10b applies in relation to assessing the adequacy of intake for mixed
population groups; Tables 1114 apply to the four categories of homogeneous groups of
ADF members.
When determining the adequacy of nutritional intake of an individual ADF member, it is
appropriate to use the MRDIs applicable to that individuals population group and
activity category (Tables 58 apply).
The recommended entitlements in this report are also considered to be an appropriate
basis for the development of military core food groups and a military guide to healthy
eating.
It is also suggested that the nutritional entitlements supporting hot-boxed meals (used
for fresh feeding in the field) should be based on the appropriate work category (3 or
above) for adult male ADF members.
The implications of under-consumption in the field, specifically when feeding is by CRP,
are addressed. The origins of negative energy balance, how this affects military
performance, and steps that may be taken in an attempt to overcome any perceived
problems are critical factors affecting nutritional status of ADF members. It is concluded
that previously well-nourished troops should suffer no decrement to performance for at
least 16 days when rationing is solely by CRP. It is also concluded that more research is
needed in this area.
Following an extended period of negative energy balance, it may be appropriate to aim for
a recovery period equal to about half the period of negative energy balance. Until further
information is available, it is considered prudent to attempt to limit the rate at which
recovery is attained to a maximum of ~8 MJ per day. That is, the tentative
recommendation is that the excess of intake over expenditure during the recovery period
should be no more than 8 MJ per day. It may also be appropriate to seek advice from
military Medical Officers on how recovery feeding can be safely conducted if troops have
undergone an extensive period of severe under-consumption.&lt;/p&gt;
</description>
	<link>http://www.dsto.defence.gov.au/publications/scientific_record.php?record=9903/</link>
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