Upgraded design methodology for airframe/engine integrated full-waverider vehicle considering thrust chamber design

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Engineering, Aerospace Engineering, Physics +11

Exhaust Nozzle Contour for Optimum Thrust

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Engineering, Aerospace Engineering, Mechanical Engineering +14

Design of Three-Dimensional Hypersonic Inlets with Rectangular-to-Elliptical Shape Transition

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Engineering, Aerospace Engineering, Mechanical Engineering +17

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Engineering, Aerospace Engineering, Systems Engineering +14

Experimental Testing of a Hypersonic Inlet with Rectangular-to-Elliptical Shape Transition

Michael K. Smart · Journal of Propulsion and Power · 2001 · 121 citations

Engineering, Aerospace Engineering, Aerodynamics +16