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Showing results for "TUNNELS"
2,002 results found - Page 41 of 84
Combined Cycle Engine (CCE) Test in 10 x 10 Supersonic Wind Tunnel
B-32 Model Close Up. Test conducted in the NACA 19 foot pressure tunnel LMAL-38560 NACA document.
Gun Turrets of XP-35. Test conducted in the NACA 19 foot pressure tunnel LMAL-38560 NACA document.
Wright Flyer Replica Test-40-0047: 40 x 80 ft. Wind Tunnel.
Gun turrets of XP-35. Test conducted in the NACA 19 foot pressure tunnel LMAL-38560 NACA document.
B-32 Model Close Up, Test conducted in the NACA 19 foot pressure tunnel LMAL-38560 NACA document.
Galileo Probe test-358 in NASA Ames Research Center12ft Pressure Wind Tunnel
UNSTART PROGRAM - 10X10 FOOT SUPERSONIC WIND TUNNEL AS PART OF THE HIGH SPEED RESEARCH PROGRAM
MODEL OF NACA Ames Research Center's 40 BY 80 FOOT SUBSONIC WIND TUNNEL.
XV-3 in Ames Reseach Center 40x80ft wind tunnel; Rotor dynamic stability tests
Mars Science Laboratory, MSL Flexible Canopy Test in the Glenn Research Center, 10x10 Supersonic Wind Tunnel
Crew Exploration Vehicle CEV-26AA with service module in 11_foot NASA Ames Transonic Wind Tunnel Test-11-0197
Wright Flyer Replica Test-40-0047: 40 x 80 ft. Wind Tunnel.
VSTOL Fighter Model in the NASA Ames 40x80ft Subsonic Wind Tunnel. Test-537 with Mike Falarski & Ray Hafalia
British royalty visits Ames; Prince Andrew, Duke of York on tour of 80x120ft Wind Tunnel
B-32 Model Close Up. Test conducted in the NACA 19 foot pressure tunnel LMAL-38560 NACA document.
Lear Jet in 40 x 80 ft. Wind Tunnel with Ed Varrette. Angle of Attack=40 degrees.
ROCKET BASED COMBINED CYCLE - RBCC - RIG 3.1 MODEL INSTALLED IN 10X10 FOOT SUPERSONIC WIND TUNNEL TEST SECTION
Facility Aerodynamic Validation and Operational Research (FAVOR) aircraft model hardware in 8x6 Supersonic Wind...
Space Shuttle Orbitor model 140 A/B-OA87 testing in the 3.5ft Hypersonic Wind Tunnel
NACA Ames Research Center's 6x6ft Supersonic Wind Tunnel compressor, showing rotor blades
Air-Breathing Propulsion - General Electric Open Rotor Model in the 8x6-Foot Supersonic Wind Tunnel
XV-15 Rotor Installation in 80X120 ft. Wind Tunnel Test-0048. Noise Reduction
B-32 Model Close Up. Test conducted in the NACA 19 foot pressure tunnel LMAL-38560 NACA document.