Test to obtain acoustic data on jet interactions of plume simulations with separation aerodynamic effects for selected specific conditions.
Force, moment, and pressure data measurements of the aerodynamic effects on the inboard underside of the wing near the nacelle…
3% space shuttle launch configuration; super light weight (SLWT) external tank with protuberances, orbiter, and RSRB’s.
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.
