Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90713/1/AIAA-2011-5756-100.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83559/1/AIAA-46521-633.pd
A model of a scramjet inlet was investigated experimentally in the hypersonic wind tunnel H2K of DLR...
This work represents an initial attempt to determine what, if any, issues arise from scaling demonst...
The experimental low-speed aerodynamic characteristics of an axisymmetric mixed-compression superson...
We conducted an extensive experimental examination of the operational behavior of a three-dimensiona...
A new methodology has been developed for the design of hypersonic scramjet inlets using\ud gas dynam...
The study concerns the propagation of shockwaves within an inlet of a scramjet engine and effect of ...
The performance of candidate supersonic cruise inlets is reviewed and the aerodynamic installation p...
A new methodology has been developed for the design of hypersonic scramjet inlets using gas dynamic ...
Concepts are investigated for obtaining both low cowl drag and good inlet performance at high angles...
Design effects on performance of two dimensional mixed-compression supersonic inlets with low angle ...
A new methodology has been developed for the design of hypersonic scramjet inlets using gas dynamic ...
A computational study was performed to explore the aerodynamic performance of a streamline-traced, e...
Several variable geometry high Mach inlet concepts, aimed at meeting a system noise objective of 15 ...
A brief summary is made of the performance of a series of variable-geometry type scoop inlets invest...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83559/1/AIAA-46521-633.pd
A model of a scramjet inlet was investigated experimentally in the hypersonic wind tunnel H2K of DLR...
This work represents an initial attempt to determine what, if any, issues arise from scaling demonst...
The experimental low-speed aerodynamic characteristics of an axisymmetric mixed-compression superson...
We conducted an extensive experimental examination of the operational behavior of a three-dimensiona...
A new methodology has been developed for the design of hypersonic scramjet inlets using\ud gas dynam...
The study concerns the propagation of shockwaves within an inlet of a scramjet engine and effect of ...
The performance of candidate supersonic cruise inlets is reviewed and the aerodynamic installation p...
A new methodology has been developed for the design of hypersonic scramjet inlets using gas dynamic ...
Concepts are investigated for obtaining both low cowl drag and good inlet performance at high angles...
Design effects on performance of two dimensional mixed-compression supersonic inlets with low angle ...
A new methodology has been developed for the design of hypersonic scramjet inlets using gas dynamic ...
A computational study was performed to explore the aerodynamic performance of a streamline-traced, e...
Several variable geometry high Mach inlet concepts, aimed at meeting a system noise objective of 15 ...
A brief summary is made of the performance of a series of variable-geometry type scoop inlets invest...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83559/1/AIAA-46521-633.pd
A model of a scramjet inlet was investigated experimentally in the hypersonic wind tunnel H2K of DLR...
This work represents an initial attempt to determine what, if any, issues arise from scaling demonst...
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