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Showing results for "TUNNELS"
2,007 results found - Page 44 of 84
Historical Baseline Blade Set (F31/A31) Installed on the Open Rotor Propulsion Rig in the 9x15 Wind Tunnel
Space Shuttle Orbitor model 140 A/B-OA87 testing in the 3.5ft Hypersonic Wind Tunnel
ALLISON LOW SPEED NOISE FAN WITH SWEPT / LEANED STATORS IN 9X15 FOOT LOW SPEED WIND TUNNEL
Common Research Model, CRM, in the Icing Research Tunnel, IRT, Installation of Test Hardware
Army/Sikorsky Active Rotor Test TR40-019 in teh 40x80ft wind tunnel at Ames Research Center.
Construction of the Ames Full-Scale 40x80ft Wind tunnel. - side view of entrance cone, blimp in background
IMX (Inlet Mode Transistion) Mach 4 Inlet Model in the 1x1 Wind Tunnel
ADM Swept Tip Rotor with Brian Chan in 7 x 10 ft# 1 Wind Tunnel Test-7101099.
Lockheed AH-56 Helicopter; Cheyenne, 40 x 80 ft. Wind Tunnel. (3/4 rear view)
Historical Baseline Blade Set (F31/A31) Installed on the Open Rotor Propulsion Rig in the 9x15 Wind Tunnel
NACA Ames Research Center 7x10_foot Wind Tunnel test of the Douglas XSB2D-1 model
Lear Jet in 40 x 80 ft. Wind Tunnel with Ed Varrette. Angle of Attack=0 degrees.
Publicity Photos of Bell Computing Machines at 19 Foot Pressure Tunnel Mrs. Doris Rudd Porter Baron photographed in...
ADM Swept Tip Rotor in 7 x 10 ft. # 1 Wind Tunnel Test-7101099.
Facility Aerodynamic Validation and Operational Research (FAVOR) aircraft model hardware in 8x6 Supersonic Wind...
Detail Shots of B-32 Turret. 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.
H-126 (Hunting) Jet Flap Aircraft: 40 x 80 ft. Wind Tunnel Test Program, B. Reuben.
Detail Shots of B-32 Turret. Test conducted in the NACA 19 foot pressure tunnel LMAL-38560 NACA document.
SCAT (Supersonic Commercial Air Transport) 15F, Test-332 in 40x80ft. Wind Tunnel
NORTHROP GRUMMAN NOISE REDUCTION TEST 1996 9X15 FOOT WIND TUNNEL ENTRY
UNSTART PROGRAM - 10X10 FOOT SUPERSONIC WIND TUNNEL AS PART OF THE HIGH SPEED RESEARCH PROGRAM
B-32 Model Close Up. Test conducted in the NACA 19 foot pressure tunnel LMAL-38560 NACA document.
NASA Ames Research Center's 1x3 1/2 ft wind tunnel (to illustrate 1946 budget)