Add to ORKGInteraction of nacelle-mounted supersonic propulsion system with simulated wing boundary laye
The flow field near four small-scale ducted-nacelle bodies of revolution has been analytically and e...
Ultra high-bypass ratio aircraft engines adopt slim fan cowl profiles which are sensitive to separat...
One of the propulsion system concepts to be considered for the High-Speed Civil Transport (HSCT) is ...
A flow visualization study was made in the 9 x 9 inch supersonic wind tunnel at Wichita State Univer...
An investigation was made to assess the effect of wing-mounted nacelles on a supercritical wing conf...
Detailed interference force-and-pressure data were obtained on a representative supersonic transport...
Wind tunnel tests to determine the effect of engine nacelles added to a low wing fuselage vertical t...
Data from wind tunnel tests of a powered propeller and nacelle mounted on a supercritical wing are a...
Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing en...
Experimental tests have been conducted to determine possible aerodynamic interference effects due to...
An experimental investigation has been made of the boundary layer flow in a supersonic axisymmetric ...
Effects of turbojet engine unstart on engine operation and characteristics of stall propagation thro...
The installation interference effects of an underwing-mounted, long duct, turbofan nacelle were eval...
An approximately 1/30th-scale model of a CTOL aircraft designed for efficient cruise between Mach 0....
A Mach 5 cruise aircraft was studied in a joint program effort. The propulsion system chosen for thi...
The flow field near four small-scale ducted-nacelle bodies of revolution has been analytically and e...
Ultra high-bypass ratio aircraft engines adopt slim fan cowl profiles which are sensitive to separat...
One of the propulsion system concepts to be considered for the High-Speed Civil Transport (HSCT) is ...
A flow visualization study was made in the 9 x 9 inch supersonic wind tunnel at Wichita State Univer...
An investigation was made to assess the effect of wing-mounted nacelles on a supercritical wing conf...
Detailed interference force-and-pressure data were obtained on a representative supersonic transport...
Wind tunnel tests to determine the effect of engine nacelles added to a low wing fuselage vertical t...
Data from wind tunnel tests of a powered propeller and nacelle mounted on a supercritical wing are a...
Wind tunnel tests of airframe installation effects on F-106B scale model with simulated underwing en...
Experimental tests have been conducted to determine possible aerodynamic interference effects due to...
An experimental investigation has been made of the boundary layer flow in a supersonic axisymmetric ...
Effects of turbojet engine unstart on engine operation and characteristics of stall propagation thro...
The installation interference effects of an underwing-mounted, long duct, turbofan nacelle were eval...
An approximately 1/30th-scale model of a CTOL aircraft designed for efficient cruise between Mach 0....
A Mach 5 cruise aircraft was studied in a joint program effort. The propulsion system chosen for thi...
The flow field near four small-scale ducted-nacelle bodies of revolution has been analytically and e...
Ultra high-bypass ratio aircraft engines adopt slim fan cowl profiles which are sensitive to separat...
One of the propulsion system concepts to be considered for the High-Speed Civil Transport (HSCT) is ...