Mode Transition Design Considerations for an Airbreathing Combined-Cycle Hypersonic Vehicle Peter J Ouzts NASA Glenn Research Center Brookpark, OH

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Date: 2010-04-13 11:30:19 Fluid dynamics Aviation Aerodynamics Aircraft engines Single-stage-to-orbit Scramjet Hypersonic speed Ramjet Rocket-based combined cycle Jet engines Aerospace engineering Spacecraft propulsion		Mode Transition Design Considerations for an Airbreathing Combined-Cycle Hypersonic Vehicle Peter J Ouzts NASA Glenn Research Center Brookpark, OH Add to Reading List Source URL: hapb-www.larc.nasa.gov Download Document from Source Website File Size: 507,68 KB Share Document on Facebook

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