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Hypersonic lateral and directional stability characteristics of Aeroassist Flight Experiment configuration in air and CF4 — ReaderExpo

Hypersonic lateral and directional stability characteristics of Aeroassist Flight Experiment configuration in air and CF4

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Hypersonic lateral and directional stability characteristics of Aeroassist Flight Experiment configuration in air and CF4

by John R. Micol

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Aeroassist Flight ExperimentStability tests

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Stagnation-point heat-transfer rate predictions at aeroassist flight conditions

Roop N. Gupta

Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction

John R. Micol

Prediction of the pattern performance for the Aeroassist Flight Experiment (AFE) spacecraft

C. Yang

Surface flow and heating distributions on a cylinder in near wake of Aeroassist Flight Experiment (AFE) configuration at incidence in Mach 10 air

William L. Wells