Add to ORKGSimulated wing effect on pressure drag coefficient of subsonic boattail at angle of attac
Experimental side and bade pressure distributions over a series of conical boattails without and wit...
The influence of upper-surface nacelle exhaust flow on the aerodynamic characteristics of a superson...
Wind tunnel tests to determine the effect of engine nacelles added to a low wing fuselage vertical t...
Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodies of supersoni...
Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing en...
Airframe installation effects on variable flap ejector nozzle of underwing engine nacell
A circular-arc - conic boattail nozzle, typical of those used on a twin engine fighter, was tested o...
Four configurations of rounded shoulder boattail nozzles were tested on an underwing nacelle mounted...
A contoured boattail nozzle typical of those used on a twin-engine fighter was tested on an underwin...
An experimental investigation was conducted in the AEDC 16-foot Transonic Wind Tunnel (16T) to deter...
An investigation was conducted in a transonic cryogenic tunnel to determine the effect of varying Re...
Jet effects on boattail pressure drag of isolated ejector nozzles at Mach 0.60 to 1.4
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
Several variations of a boattailed shroud for a 10 deg conical plug nozzle were tested using an F-10...
Jet effects on boattail axial force of conical afterbodies at subsonic and transonic speed
Experimental side and bade pressure distributions over a series of conical boattails without and wit...
The influence of upper-surface nacelle exhaust flow on the aerodynamic characteristics of a superson...
Wind tunnel tests to determine the effect of engine nacelles added to a low wing fuselage vertical t...
Effect of boattail juncture shape on pressure drag coefficients of isolated afterbodies of supersoni...
Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing en...
Airframe installation effects on variable flap ejector nozzle of underwing engine nacell
A circular-arc - conic boattail nozzle, typical of those used on a twin engine fighter, was tested o...
Four configurations of rounded shoulder boattail nozzles were tested on an underwing nacelle mounted...
A contoured boattail nozzle typical of those used on a twin-engine fighter was tested on an underwin...
An experimental investigation was conducted in the AEDC 16-foot Transonic Wind Tunnel (16T) to deter...
An investigation was conducted in a transonic cryogenic tunnel to determine the effect of varying Re...
Jet effects on boattail pressure drag of isolated ejector nozzles at Mach 0.60 to 1.4
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
Several variations of a boattailed shroud for a 10 deg conical plug nozzle were tested using an F-10...
Jet effects on boattail axial force of conical afterbodies at subsonic and transonic speed
Experimental side and bade pressure distributions over a series of conical boattails without and wit...
The influence of upper-surface nacelle exhaust flow on the aerodynamic characteristics of a superson...
Wind tunnel tests to determine the effect of engine nacelles added to a low wing fuselage vertical t...