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Showing results for "Blade"
189 results found - Page 3 of 8
JVX/ATB Rotor Blade Project: Bell Boeing Rotor for the XV-15 tilt rotor Research Aircraft (TRRA)
JVX/ATB Rotor Blades Test; OARF Static Test Stand N-249.
JVX/ATB Rotor Blades Test; OARF Static Test Stand N-249.
JVX/ATB Rotor Blades Test; OARF Static Test Stand N-249.
Historical Baseline Blade Set (F31/A31) Installed on the Open Rotor Propulsion Rig in the 9x15 Wind Tunnel
Energy Efficient Engine (EEE) Tip Clearance Static Pressure Measurement Blades for CW-22
Composite Blade Test 11 ft. Wind Tunnel (Test-194-1-11).
Historical Baseline Blade Set (F31/A31) Installed on the Open Rotor Propulsion Rig in the 9x15 Wind Tunnel
JVX/ATB Rotor Blades Test; OARF Static Test Stand N-249.
JVX/ATB Rotor Blades Test; OARF Static Test Stand N-249.
JVX/ATB Rotor Blades Test; OARF Static Test Stand N-249.
JVX/ATB Rotor Blades Test; OARF Static Test Stand N-249.
JVX/ATB Rotor Blade Project: Bell Boeing Rotor for the XV-15 tilt rotor Research Aircraft (TRRA)
NASA/Army UH-60 Individual Blade Control (IBC) test on LRTA in 40x80ft. Wind Tunnel at Ames Research Center
Composite Blade Test 11 ft. Wind Tunnel (Test-194-1-11).
3/4 front view of the Lockheed Stopped Rotor with blades unfolded. Charles Greco and Ed Verrette in photo.
Ultra Efficient Engine Technology (UEET) W-7 2-Stage Proof of Concept Compressor - Blade Tip Clearance Sensor...
UH-60 Blackhawk (NASA 748) and YO-3A (NASA-718) inflight over Altamont Pass, CA - Blade Vortex Interaction Noise...
VSHAIP test in 7x10ft#1 W.T. (multiple model configruations) V-22 helicopter shipboard aerodynamic interaction...
JVX/ATB Rotor Blade Project: Bell Boeing Rotor for the XV-15 tilt rotor Research Aircraft (TRRA) and test crew in...
VSHAIP test in 7x10ft#1 W.T. (multiple model configruations) V-22 helicopter shipboard aerodynamic interaction...
VSHAIP test in 7x10ft#1 W.T. (multiple model configruations) V-22 helicopter shipboard aerodynamic interaction...
VSHAIP test in 7x10ft#1 W.T. (multiple model configruations) V-22 helicopter shipboard aerodynamic interaction...
Ultra Efficient Engine Technology (UEET) W-7 2-Stage Proof of Concept Compressor - Blade Tip Clearance Sensor...