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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

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