Add to ORKGApproximation of ramjet exhaust plume effects on external pressure of nozzle extension of X-15 aircraf
An experimental aerodynamic investigation was conducted to provide data for studies to determine the...
Newly emerging aerospace technology points to the feasibility of sustained hypersonic flight. Design...
Two aft underwing nacelles housing afterburning J85 engines were added to an F106 to study exhaust n...
Wind tunnel study of flow field beneath X-15 aircraft fuselage at supersonic to hypersonic speed
Flow field around pylon-mounted dummy ramjet engine of X-15-2 airplane prior to hypersonic ramjet en...
Underexpanded rocket nozzle exhaust plumes impinging upon perpendicular flat surfac
A parametric experimental investigation of a scramjet nozzle was conducted with a gas mixture used t...
Investigation of engine-exhaust-airframe interference on cruise vehicle at Mach
An investigation of the jet-spreading characteristics of a 16 inch ram-jet engine was conducted in t...
An investigation was conducted to determine the effect of varying the jet exhaust ratio of specific ...
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers ...
Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf
Static pressure coefficient distributions on the forebody, afterbody, and nozzles of a 1/12 scale F-...
A pitot-rake survey of the simulated exhaust of a half-span scramjet nozzle model was conducted in t...
Results from an investigation of the effects of underexpanded engine exhaust flow on the aerodynamic...
An experimental aerodynamic investigation was conducted to provide data for studies to determine the...
Newly emerging aerospace technology points to the feasibility of sustained hypersonic flight. Design...
Two aft underwing nacelles housing afterburning J85 engines were added to an F106 to study exhaust n...
Wind tunnel study of flow field beneath X-15 aircraft fuselage at supersonic to hypersonic speed
Flow field around pylon-mounted dummy ramjet engine of X-15-2 airplane prior to hypersonic ramjet en...
Underexpanded rocket nozzle exhaust plumes impinging upon perpendicular flat surfac
A parametric experimental investigation of a scramjet nozzle was conducted with a gas mixture used t...
Investigation of engine-exhaust-airframe interference on cruise vehicle at Mach
An investigation of the jet-spreading characteristics of a 16 inch ram-jet engine was conducted in t...
An investigation was conducted to determine the effect of varying the jet exhaust ratio of specific ...
Measured and calculated flow conditions on forward fuselage of X-15 plane and model at Mach numbers ...
Flow distribution in flight test and wind tunnel hypersonic flow of X-15 aircraf
Static pressure coefficient distributions on the forebody, afterbody, and nozzles of a 1/12 scale F-...
A pitot-rake survey of the simulated exhaust of a half-span scramjet nozzle model was conducted in t...
Results from an investigation of the effects of underexpanded engine exhaust flow on the aerodynamic...
An experimental aerodynamic investigation was conducted to provide data for studies to determine the...
Newly emerging aerospace technology points to the feasibility of sustained hypersonic flight. Design...
Two aft underwing nacelles housing afterburning J85 engines were added to an F106 to study exhaust n...