Add to ORKGSupersonic performance of variable two-dimensional inlets designed for engine-inlet matching
An analysis of the nose-inlet shapes developed in previous investigations to represent the optimum f...
An experimental investigation was conducted to determine the performance characteristics an underslu...
Jet engine induction systems investigations and relationship of air inlets, drag, airframe, pressure...
Air inlet for turbojet engines having variable angle two-dimensional compression surface and fixed-g...
An analysis of inlet-turbojet-engine matching for a range of Mach numbers up to 2.0 indicates large ...
Pressure recovery in adjustable supersonic inlet combined with j34 turbojet engine up to mach 2.0
Internal flow performance of fixed 14 deg ramp inlet from zero to 20 deg angle of attack at superson...
Translating spike inlet air flow regulation characteristics from transonic to supersonic speeds at z...
Control of variable-geometry inlets at constant mach numbers with blunt lip diffuser
Wedge and scoop air inlet performance and thrust minus drag comparisons at free stream in supersonic...
An extensive program was undertaken to investigate the effect of several geometric variables on the ...
Pressure distribution at supersonic speeds on conically cambered wing with and without pylon mounted...
A general discussion of the air-inlet problem is presented. Recently obtained drag and pressure-reco...
Performance of four experimentally investigated axially symmetric spike-type nose inlets is compared...
A method of presenting turbojet-engine air-flow requirements and inlet-system air-flow capacities in...
An analysis of the nose-inlet shapes developed in previous investigations to represent the optimum f...
An experimental investigation was conducted to determine the performance characteristics an underslu...
Jet engine induction systems investigations and relationship of air inlets, drag, airframe, pressure...
Air inlet for turbojet engines having variable angle two-dimensional compression surface and fixed-g...
An analysis of inlet-turbojet-engine matching for a range of Mach numbers up to 2.0 indicates large ...
Pressure recovery in adjustable supersonic inlet combined with j34 turbojet engine up to mach 2.0
Internal flow performance of fixed 14 deg ramp inlet from zero to 20 deg angle of attack at superson...
Translating spike inlet air flow regulation characteristics from transonic to supersonic speeds at z...
Control of variable-geometry inlets at constant mach numbers with blunt lip diffuser
Wedge and scoop air inlet performance and thrust minus drag comparisons at free stream in supersonic...
An extensive program was undertaken to investigate the effect of several geometric variables on the ...
Pressure distribution at supersonic speeds on conically cambered wing with and without pylon mounted...
A general discussion of the air-inlet problem is presented. Recently obtained drag and pressure-reco...
Performance of four experimentally investigated axially symmetric spike-type nose inlets is compared...
A method of presenting turbojet-engine air-flow requirements and inlet-system air-flow capacities in...
An analysis of the nose-inlet shapes developed in previous investigations to represent the optimum f...
An experimental investigation was conducted to determine the performance characteristics an underslu...
Jet engine induction systems investigations and relationship of air inlets, drag, airframe, pressure...