3% space shuttle launch configuration; super light weight (SLWT) external tank with protuberances, orbiter, and RSRB's.
To test force, moment, and pressure data measurements of the jet interference effects on the crew exploration vehicle (CEV) alternate…
To test force, moment, and pressure data measurements of the jet interference effects on the crew exploration vehicle (CEV) alternate…
A model of f-18 is tested in the NASA Ames 11-by 11-foot transonic wind tunnel.
A model of F-18 is tested in the NASA Ames 11-by 11-foot transonic wind tunnel.Image credit: NASA Ames Research Center
Test to investigate aerodynamic proximity and jettison motor plume interaction effects on the separation of the crew module from the…
Wind tunnel test to calibrate the flow-around balance model assembly for momentum corrections.
Model of Crew Exploration Vehicle (CEV) with pressure sensitive paint (PSP) to obtain data on jet interactions of plume effects…
Low boom passenger airline concept to obtain force and pressure measurements and calibrate computational fluid dynamics (CFD) tools estimates.
Low boom passenger airline concept to obtain force and pressure measurements and calibrate computational fluid dynamics (CFD) tools estimates.
