LASER Velocimetry System for Flow Measurement.  Advanced Short Takeoff and Vertical Landing, ASTOVL model n the 9x15 foot Low Speed Wind Tunnel, LSWT
GRC-1994-C-00160
Supersonic Short Take Off Vertical Landing Hot Gas Ingestion Model Testing in the 9x15-foot Low Speed Wind Tunnel, LSWT
GRC-1993-C-07355
The 9x15 low speed tunnel tests take off and landing of aircraft.  The laser velocimetry system for flow measurement show here, with the color blue and green lasers, measures engine exhaust that comes back up from the ground.  The STOVL model n the 9x15 low speed wind tunnel, building 39, is similar to the British Harrier aircraft.
STOVL (Short Take Off Vertical Landing) Phase III Hot Gas Ingestion Into Engine Intake Test in the 9x15 Low Speed Wind Tunnel
Ultra High Bypass Integrated System Test Testing of an Ultra High Bypass Ratio Turbofan model in the 9-by 15-Foot Low Speed Wind Tunnel. Pratt & Whitney designed the experimental engine to meet new efficiency and noise reduction targets for commercial aircraft set by NASA and the Federal Aviation Administration. The 9-by 15 tests analyzed two noise reduction technologies.
Ultra High Bypass Ratio Turbofan model in the 9-by 15-Foot Low Speed Wind Tunnel