NASA Scientific and Technical Aerospace Reports
NASA Scientific and Technical Aerospace Reports
NASA Scientific and Technical Aerospace Reports
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The Kirchhoff Formula for a Supersonically<br />
Moving Surface – 288<br />
AEROASSIST<br />
Atmospheric Models for Aeroentry <strong>and</strong><br />
Aeroassist – 24<br />
AEROBRAKING<br />
Atmospheric Models for Aerocapture<br />
Systems Studies – 322<br />
Atmospheric Models for Aeroentry <strong>and</strong><br />
Aeroassist – 24<br />
AEROCAPTURE<br />
Aerocapture Performance Analysis for a<br />
Neptune-Triton Exploration Mission<br />
– 320<br />
Atmospheric Models for Aerocapture<br />
Systems Studies – 322<br />
Atmospheric Models for Aeroentry <strong>and</strong><br />
Aeroassist – 24<br />
Neptune Aerocapture Systems Analysis<br />
– 23<br />
Preliminary Convective-Radiative Heating<br />
Environments for a Neptune Aerocapture<br />
Mission – 25<br />
Structural Design for a Neptune Aerocapture<br />
Mission – 40<br />
AERODYNAMIC CHARACTERISTICS<br />
Aerodynamic Performance <strong>and</strong> Flow-<br />
Field Characteristics of Two Waverider-<br />
Derived Hypersonic Cruise Configurations<br />
– 110<br />
An Experimental Study Synthetic Jets<br />
from Rectangular Orifices – 3<br />
Hypersonic Aerodynamic Characteristics<br />
of a Proposed Single-Stage-To-Orbit Vehicle<br />
– 11<br />
AERODYNAMIC COEFFICIENTS<br />
Effects of Sonic Line Transition on Aerothermodynamics<br />
of the Mars Pathfinder<br />
Probe – 2<br />
AERODYNAMIC CONFIGURATIONS<br />
Aerodynamic Performance <strong>and</strong> Flow-<br />
Field Characteristics of Two Waverider-<br />
Derived Hypersonic Cruise Configurations<br />
– 110<br />
Airfoil Design <strong>and</strong> Optimization by the<br />
One-Shot Method – 109<br />
Grid Sensitivity <strong>and</strong> Aerodynamic Optimization<br />
of Generic Airfoils – 10<br />
Navier-Stokes Computations <strong>and</strong> Experimental<br />
Comparisons for Multielement<br />
Airfoil Configurations – 109<br />
Transonic Navier-Stokes Solutions about<br />
a Complex High-Speed Accelerator Configuration<br />
– 119<br />
AERODYNAMIC HEATING<br />
Hypervelocity Aeroheating Measurements<br />
in Wake of Mars Mission Entry<br />
Vehicle – 112<br />
AERODYNAMIC LOADS<br />
Fatigue Life Estimate of Centre-Box Lug<br />
in Seahawk’s Stabilator – 78<br />
A-2<br />
AERODYNAMIC NOISE<br />
Active Control of Fan-Generated Tone<br />
Noise – 288<br />
The Kirchhoff Formula for a Supersonically<br />
Moving Surface – 288<br />
AERODYNAMICS<br />
Characteristics of a Cambered Circulation<br />
Control Airfoil Having Both Upper<br />
<strong>and</strong> Lower Surface Trailing Edge<br />
Slots – 3<br />
Research Engineering – 329<br />
AEROELASTICITY<br />
Control of Systems With Periodic Coefficients,<br />
With Application To Active Rotor<br />
Control – 2<br />
AERONAUTICAL ENGINEERING<br />
<strong>NASA</strong> Programs in Advanced Sensors<br />
<strong>and</strong> Measurement Technology for Aeronautical<br />
Applications – 16<br />
AEROSHELLS<br />
Neptune Aerocapture Systems Analysis<br />
– 23<br />
AEROSOLS<br />
CuInS2 Films Deposited by Aerosol-<br />
Assisted Chemical Vapor Deposition Using<br />
Ternary Single-Source Precursors<br />
– 50<br />
Global <strong>and</strong> Regional Decreases in Tropospheric<br />
Oxidants from Photochemical<br />
Effects of Aerosols – 149<br />
Interannual <strong>and</strong> Seasonal Variability of<br />
Biomass Burning Emissions Constrained<br />
by Satellite Observations – 148<br />
Preliminary Evaluation of the Impacts of<br />
Aerosol Particles on Laser Performance<br />
in the Coastal Marine Boundary<br />
Layer – 129<br />
AEROSPACE ENGINEERING<br />
Advanced Materials <strong>and</strong> Coatings for<br />
<strong>Aerospace</strong> Applications – 54<br />
Introduction - MEMS <strong>Aerospace</strong> Applications<br />
– 99<br />
Making Tracks at JPL – 322<br />
OAST Technology for the Future. Executive<br />
Summary – 22<br />
OAST Technology for the Future. Volume<br />
2 - Critical Technologies, Themes<br />
1-4 – 22<br />
OAST Technology for the Future. Volume<br />
3 - Critical Technologies, Themes<br />
5-8 – 21<br />
AEROSPACE ENVIRONMENTS<br />
AF-Geospace 2.0 – 238<br />
An Improved Method for Simulating the<br />
Charge of Dielectrics in a Charging Electron<br />
Environment – 98<br />
Electron Emission Properties of Insulator<br />
Materials Pertinent to the International<br />
Space Station – 35<br />
Miniaturization Science for Space: Lubrication<br />
of Micro-Electro-Mechanical Systems<br />
(MEMS) for Space Environments<br />
– 318<br />
New <strong>NASA</strong> SEE LEO Spacecraft Charging<br />
Design Guidelines: How to Survive in<br />
LEO Rather than GEO – 32<br />
OAST Technology for the Future. Executive<br />
Summary – 22<br />
OAST Technology for the Future. Volume<br />
2 - Critical Technologies, Themes<br />
1-4 – 22<br />
OAST Technology for the Future. Volume<br />
3 - Critical Technologies, Themes<br />
5-8 – 21<br />
Space Environmental Effects <strong>and</strong> Spacecraft<br />
EMC – 42<br />
The Electric Propulsion Interactions<br />
Code (EPIC) – 238<br />
The Viability of Using Weight-Saving Material<br />
for Future Long-Term Space Vehicles<br />
(i.e., Satellites) – 52<br />
AEROSPACE MEDICINE<br />
Line Pilots’ Attitudes about <strong>and</strong> Experience<br />
with Flight Deck Automation: Results<br />
of an International Survey <strong>and</strong> Proposed<br />
Guidelines – 225<br />
AEROSPACE PLANES<br />
A Flight Control Approach for Small Reentry<br />
Vehicles – 41<br />
AEROSPACE SAFETY<br />
Shuttle Systems 3-D Applications: Application<br />
of 3-D Graphics in Engineering<br />
Training for Shuttle Ground Processing<br />
– 27<br />
AEROSPACE SCIENCES<br />
SCDM in a Distributed Environment<br />
– 240<br />
AEROSPACE SYSTEMS<br />
ECSS-E-20-06 Draft St<strong>and</strong>ard on Spacecraft<br />
Charging: Environment-Induced Effects<br />
on the Electrostatic Behaviour of<br />
Space Systems – 316<br />
<strong>NASA</strong> Langley Research <strong>and</strong><br />
Technology-Transfer Program in Formal<br />
Methods – 306<br />
AEROSPACE VEHICLES<br />
Leo Spacecraft Charging Design Guidelines:<br />
A Proposed <strong>NASA</strong> St<strong>and</strong>ard – 41<br />
Secondary Electron Emission Causing<br />
Potential Barriers Around Negatively<br />
Charged Spacecraft – 37<br />
The Viability of Using Weight-Saving Material<br />
for Future Long-Term Space Vehicles<br />
(i.e., Satellites) – 52<br />
Unmanned Aerial Vehicles: Implications<br />
for Military Operations – 13<br />
AEROSPIKE ENGINES<br />
Experimental Results on the Feasibility<br />
of an Aerospike for Hypersonic Missiles<br />
– 10<br />
AEROTHERMODYNAMICS<br />
Dual-Code Solution Strategy for<br />
Chemically-Reacting<br />
Flows – 109<br />
Hypersonic<br />
Effects of Sonic Line Transition on Aerothermodynamics<br />
of the Mars Pathfinder<br />
Probe – 2