Two scaled models of the Aeroassist Flight Experiment (AFE) vehicle were tested in two air wind tunnels and one CF4 tunnel. The tests were to determine the static longitudinal aerodynamic characteristics, and shock shapes for the configuration in hypersonic continuum flow. The tests were conducted with a range of angle of attack to evaluate the effects of Mach number, Reynolds numbers, and normal shock density ratio.
Measured and predicted aerodynamic coefficients and shock shapes for Aeroassist Flight Experiment (AFE) configuration
1989-01-01
Report
No indication
English
Aeroassist Flight Experiment (AFE)
NTRS | 1988
|The Aeroassist Flight Experiment
NTRS | 1987
|Aeroassist Flight Experiment (AFE)
NTIS | 1988
|