NASA Scientific and Technical Aerospace Reports
NASA Scientific and Technical Aerospace Reports
NASA Scientific and Technical Aerospace Reports
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COMMAND AND CONTROL<br />
An Enemy within the System: Illustrative<br />
Examinations of C2 Questions using Distillations<br />
– 242<br />
An Overview of Romanian Comm<strong>and</strong><br />
<strong>and</strong> Control Systems – 95<br />
Analysis <strong>and</strong> Evaluation of the Immediate<br />
Reaction Task Force (L<strong>and</strong>) Comm<strong>and</strong><br />
<strong>and</strong> Control Concept: Applying the<br />
COBP – 268<br />
Digital Proficiency Levels for the Brigade<br />
<strong>and</strong> Battalion Battle Staff – 234<br />
Mixed Initiative Control of Automa-<br />
Teams, Open Experimentation Platform<br />
– 6<br />
Pilot Study: System Model of Situation<br />
Awareness <strong>and</strong> Decision Making in Comm<strong>and</strong><br />
<strong>and</strong> Control – 94<br />
Simulation Interoperability for the New<br />
RNLA C2 WorkStation – 241<br />
Technology <strong>and</strong> Comm<strong>and</strong>: Implications<br />
for Military Operations in the Twenty-First<br />
Century – 95<br />
The Relevance of Human Behaviour<br />
Representation in Future C2 Systems:<br />
Current <strong>and</strong> Future Research Approaches<br />
– 243<br />
COMMERCIAL AIRCRAFT<br />
Fuzzification of Electromagnetic Interference<br />
Patterns Onboard Commercial Airliners<br />
Due to Wireless Technology – 8<br />
Regulation, Competition <strong>and</strong> Network<br />
Evolution in Aviation – 305<br />
COMMERCIALIZATION<br />
Commercialization of CIS-Based Thin-<br />
Film PV. Final <strong>Technical</strong> Report August<br />
1998-November 2001 – 143<br />
COMMUNICATION NETWORKS<br />
Application of AirCell Cellular AMPS Network<br />
<strong>and</strong> Iridium Satellite System Dual<br />
Mode Service to Air Traffic Management<br />
– 91<br />
Harris Simulator Design Description for<br />
Adaptive Distributed Network Management<br />
System – 95<br />
IMT-2000 Satellite St<strong>and</strong>ards with Applications<br />
to Mobile Air Traffic Communications<br />
Networks – 96<br />
Mobile Router Testing with Diverse RF<br />
Communications Links – 8<br />
Range Extension Techniques Available<br />
to the Army Tactical Communications<br />
System – 97<br />
Self-Configuring Wireless Transmission<br />
<strong>and</strong> Decentralized Data Processing for<br />
Generic Sensor Networks – 269<br />
Strategic Supply – 242<br />
COMPATIBILITY<br />
Airborne <strong>and</strong> Space-Based Lasers: An<br />
Analysis of Technological <strong>and</strong> Operational<br />
Compatibility – 128<br />
A-14<br />
COMPENSATORS<br />
Model-Based Compensator <strong>and</strong> Control<br />
Design for High Performance Nonlinear<br />
Tr<strong>and</strong>ucers – 102<br />
COMPETITION<br />
A Fuzzy Approach of the Competition on<br />
Air Transport Market – 313<br />
Application of Core Theory to the U.S.<br />
Airline Industry – 305<br />
Regulation, Competition <strong>and</strong> Network<br />
Evolution in Aviation – 305<br />
COMPLEXITY<br />
Designing for Cost – 315<br />
COMPOSITE MATERIALS<br />
Accelerated Testing of Polymeric Composites:<br />
Correlation of Scale-up Effects<br />
on Viscoelastic Behavior – 58<br />
Advanced Materials <strong>and</strong> Coatings for<br />
<strong>Aerospace</strong> Applications – 54<br />
Analysis of Stainless Steel S<strong>and</strong>wich<br />
Panels with a Metal Foam Core for Lightweight<br />
Fan Blade Design – 14<br />
Effect of Sizings on the Durability of High<br />
Temperature Polymer Composites – 17<br />
Evaluation of Space Station<br />
Meteoroid/Debris Shielding Materials,<br />
Supplement – 40<br />
Modeling the Nonlinear, Strain Rate Dependent<br />
Deformation of Shuttle Leading<br />
Edge Materials with Hydrostatic Stress<br />
Effects Included – 57<br />
The Viability of Using Weight-Saving Material<br />
for Future Long-Term Space Vehicles<br />
(i.e., Satellites) – 52<br />
THERMOD Composite Airframe Termperature<br />
Prediction Tool Evaluation, Validation,<br />
<strong>and</strong> Enhancement with Initial<br />
Steady-State Temperature Data – 15<br />
Use of Advanced Composites in Maglev<br />
Guideway System – 62<br />
COMPOSITE STRUCTURES<br />
A Nonlinear Theory for Smart Composite<br />
Structures – 55<br />
A Spectral Analysis Approach for Acoustic<br />
Radiation from Composite Panels<br />
– 54<br />
Accurate Simulation of Acoustic Emission<br />
Sources in Composite Plates – 61<br />
Buckling Behavior of Compression-<br />
Loaded Composite Cylindrical Shells<br />
With Reinforced Cutouts – 136<br />
Ceramic Matrix Composite Vane Subelement<br />
Testing in a Gas Turbine Environment<br />
– 61<br />
Parametric Study on the Response of<br />
Compression-Loaded Composite Shells<br />
With Geometric <strong>and</strong> Material Imperfections<br />
– 136<br />
COMPRESSIBLE FLOW<br />
Comparison of Direct Eulerian Godunov<br />
<strong>and</strong> Lagrange Plus Remap, Artificial Viscosity<br />
Schemes – 108<br />
Very High Resolution Simulations of<br />
Compressible, Turbulent Flows – 108<br />
COMPRESSION LOADS<br />
Assessment, Development, <strong>and</strong> Validation<br />
of Computational Fracture Mechanics<br />
Methodologies <strong>and</strong> Tools for Shot-<br />
Peened Materials Used in Rotorcraft<br />
Principal Structural Elements – 9<br />
Buckling Behavior of Compression-<br />
Loaded Composite Cylindrical Shells<br />
With Reinforced Cutouts – 136<br />
Parametric Study on the Response of<br />
Compression-Loaded Composite Shells<br />
With Geometric <strong>and</strong> Material Imperfections<br />
– 136<br />
COMPUTATIONAL FLUID DYNAMICS<br />
Aerodynamic Performance <strong>and</strong> Flow-<br />
Field Characteristics of Two Waverider-<br />
Derived Hypersonic Cruise Configurations<br />
– 110<br />
Aerodynamic Performance Predictions of<br />
Single <strong>and</strong> Twin Jet Afterbodies – 113<br />
Assessing the Capability of Doppler Global<br />
Velocimetry To Measure Vortical Flow<br />
Fields – 118<br />
Computational Economy Improvements<br />
in PRISM – 108<br />
Exhaust Gas Modeling Effects on Hypersonic<br />
Powered Simulation at Mach<br />
10 – 111<br />
Experimental Results on the Feasibility<br />
of an Aerospike for Hypersonic Missiles<br />
– 10<br />
Fluidic Control of Nozzle Flow: Some<br />
Performance Measurements – 112<br />
Generic Hypersonic Inlet Module Analysis<br />
– 18<br />
Heel Removal ANalysis for Mixing<br />
Pumps of Tank 8 – 285<br />
Hypersonic Aerodynamic Characteristics<br />
of a Proposed Single-Stage-To-Orbit Vehicle<br />
– 11<br />
Hypervelocity Aeroheating Measurements<br />
in Wake of Mars Mission Entry<br />
Vehicle – 112<br />
Navier-Stokes Computations <strong>and</strong> Experimental<br />
Comparisons for Multielement<br />
Airfoil Configurations – 109<br />
Numerical Simulations Using the Immersed<br />
Boundary Technique – 111<br />
Overview 2003 of <strong>NASA</strong> Multi-D Stirling<br />
Convertor Development <strong>and</strong> DOE <strong>and</strong><br />
<strong>NASA</strong> Stirling Regenerator R <strong>and</strong> D Efforts<br />
– 46<br />
Rapid Airplane Parametric Input Design-<br />
(RAPID) – 10<br />
Simulation of Synthetic Jets in Quiescent<br />
Air Using Unsteady Reynolds Averaged<br />
Navier-Stokes Equations – 117<br />
Transonic Navier-Stokes Solutions about<br />
a Complex High-Speed Accelerator Configuration<br />
– 119<br />
Triangulation of NURBS Surfaces – 115