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Showing results for "Wind Tunnel Test"
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Wright Flyer Replica Test-40-0047: 40 x 80 ft. Wind Tunnel.
Wright Flyer Replica Test-40-0047: 40 x 80 ft. Wind Tunnel.
Q-Fan configuration in the Ames Research Center's 40x80ft. Subsonic Wind Tunnel with test engineer Mark Betzina.
X-14 NASA 704 Full Scale Airplane tests in 40x80ft. Wind Tunnel (NORMAL MOUNTING) jet inlets
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. Noise Reduction
H-126 (Hunting) Jet Flap Aircraft: 40 x 80 ft. Wind Tunnel Test Program, B. Reuben.
40x80ft wind tunnel testing of a modification to a Douglas A-26B Invader airplane (rockets, bomb and wing)
3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. (microphone set up) Noise Reduction
Mars Science Laboratory (MSL) parachuste test in the Ames 80x120ft Subsonic Wind Tunnel (TR #22 - Phase 6)
The Blue Angels crew tour the inlet of the NFAC’s 80-by-120-foot wind tunnel test section in building N221.
F-18 (12 Scale Model) 12 Foot Wind Tunnel Test-287
N-206 NASA Ames Research Center 12ft Pressure Wind Tunnel. reconstruction - test section door
CEV model with pressure sensitive paint (PSP) test 11-0148 in the 11ft Ames wind tunnel
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. Noise Reduction
0.4% Scale (SLS) Space Launch System Model Test In NASA LaRC Unitary Plan Wind Tunnel
CEV (Crew Escape Vehicle) LAS 51 aeroacoustic test-97-0186 in the Ames 9x7FT Supersonic Wind Tunnel
One-sixth scale model of Mercury space capsule model used in wind tunnel testing.
Large-Scale Low-Boom Inlet Test Single Stream Inlet in 8x6 foot Supersonic Wind Tunnel
Space Shuttle Orbitor Model (A-100) testing in the NASA Ames Research Center 40x80ft Subsonic Wind Tunnel
Model of Mercury (Redstone booster) carrying the spacecraft in the Unitary Plan wind tunnel for testing.
H-126 (Hunting) Jet Flap Aircraft: 40 x 80 ft. Wind Tunnel Test Program, B. Reuben.
Mars Science Laboratory (MSL) parachuste test in the Ames 80x120ft Subsonic Wind Tunnel (TR #22 - Phase 6)
3% Space shuttle Acoustics model test-11-150 in 11ft. wind tunnel on PAL Ramp