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Effect of Ice Shape Fidelity on Swept-Wing Aerodynamic Performance
Experimental and Computational Icing Simulation for Large Swept Wings
Comparison of Iced Aerodynamic Measurements on a Swept Wing from Two Wind Tunnels
Icing Simulation Research Supporting the Ice-Accretion Testing of Large-Scale Swept-Wing Models
Summary of Ice Shape Geometric Fidelity Studies on an Iced Swept Wing
Effect of Simulated Scalloped Ice on the Aerodynamics of a Swept-Wing at Low-Reynolds Number
Aeroacoustic Study of a Subscale Large Civil Transport (STAR) Model – Part 1: Simulations
Ares I Scale Model Acoustic Test Liftoff Acoustic Results and Comparisons
Aeroacoustic Study of a Subscale Large Civil Transport (STAR) Model – Part 1: Simulations
NASA,FAA,ONERA Swept-Wing Icing and Aerodynamics: Summary of Research and Current Status
The use of scaled dynamic models in several aerospace vehicle studies.
Thermal scale modeling techniques for Voyager-type spacecraft
Static longitudinal aerodynamic characteristics of a proposed decelerator test vehicle
Multi-Scale Modeling of Low-Density Carbon-Phenolic Ablators
Integrated Avionics System (IAS), Integrating 3-D Technology On A Spacecraft Panel
Verification of Ares I Liftoff Acoustic Environments via the Ares I Scale Model Acoustic Test
Wind Tunnel Testing of a 120th Scale Large Civil Tilt-Rotor Model in Airplane and Helicopter Modes
Feasibility study of constructing a 1/10 scale Apollo service module similitude model Final report
NASA Environmentally Responsible Aviation Hybrid Wing Body Flow-Through Nacelle Wind Tunnel CFD
NASA Environmentally Responsible Aviation Hybrid Wing Body Flow-Through Nacelle Wind Tunnel CFD
The Wind-induced Loads on a Dynamically Scaled Model of a Large Missile in Launching Position
Lunar facsimile capsule program bimonthly technical progress report no. 3, 23 feb. - 26 apr. 1963
Full-scale investigation of the aerodynamic characteristics of a model employing a sailwing concept
Water-Landing Characteristics of a 1/10-Scale Model of a Winged Missile
1/10 Scale Model Test of a Fixed Chute Mixer-Ejector Nozzle in Unsuppressed Model, Part 1
Water-landing characteristics of a 1/10-scale model of a winged missile
Advanced Modeling and Uncertainty Quantification for Flight Dynamics; Interim Results and Challenges
Dynamic model investigation of touchdown stability of lunar-landing vehicles
Some Measurements of Buffeting on an Aeroelastic Model of a Slender Wing Aircraft