Add to ORKGLongitudinal aerodynamic characteristics of twin-turbofan supersonic transport with nacelles mounted under wing
Two 0.085-scale full span wind-tunnel models of a Mach 1.60 design supercruiser configuration were t...
Airframe installation effects on variable flap ejector nozzle of underwing engine nacell
An investigation was made to assess the effect of wing-mounted nacelles on a supercritical wing conf...
Aft-fuselage-mounted nacelles effect on subsonic longitudnal aerodynamic characteristics of twin tur...
Wind tunnel tests to determine the effect of engine nacelles added to a low wing fuselage vertical t...
A 1/10-scale powered model of a twin-engine attack airplane was investigated in the Langley high-spe...
As part of a propulsion/airframe integration program, tests were conducted in the Langley 16-Foot Tr...
As part of a propulsion/airframe integration program at Langley Research Center, tests were conducte...
Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing en...
The influence of upper-surface nacelle exhaust flow on the aerodynamic characteristics of a superson...
Longitudinal aerodynamic characteristics at Mach numbers 0.50 to 1.19 of supersonic transport model ...
An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects...
An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects...
The installation interference effects of an underwing-mounted, long duct, turbofan nacelle were eval...
The arrow-wing transport configuration with detached engines located over the wing to produce upper ...
Two 0.085-scale full span wind-tunnel models of a Mach 1.60 design supercruiser configuration were t...
Airframe installation effects on variable flap ejector nozzle of underwing engine nacell
An investigation was made to assess the effect of wing-mounted nacelles on a supercritical wing conf...
Aft-fuselage-mounted nacelles effect on subsonic longitudnal aerodynamic characteristics of twin tur...
Wind tunnel tests to determine the effect of engine nacelles added to a low wing fuselage vertical t...
A 1/10-scale powered model of a twin-engine attack airplane was investigated in the Langley high-spe...
As part of a propulsion/airframe integration program, tests were conducted in the Langley 16-Foot Tr...
As part of a propulsion/airframe integration program at Langley Research Center, tests were conducte...
Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing en...
The influence of upper-surface nacelle exhaust flow on the aerodynamic characteristics of a superson...
Longitudinal aerodynamic characteristics at Mach numbers 0.50 to 1.19 of supersonic transport model ...
An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects...
An investigation has been conducted in the Langley 16-Foot Transonic Tunnel to determine the effects...
The installation interference effects of an underwing-mounted, long duct, turbofan nacelle were eval...
The arrow-wing transport configuration with detached engines located over the wing to produce upper ...
Two 0.085-scale full span wind-tunnel models of a Mach 1.60 design supercruiser configuration were t...
Airframe installation effects on variable flap ejector nozzle of underwing engine nacell
An investigation was made to assess the effect of wing-mounted nacelles on a supercritical wing conf...