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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
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Document Date: 2010-04-13 11:30:19

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File Size: 507,68 KB

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Company

Hypersonics Project 7 Modular Aero / /

IndustryTerm

propulsion systems / kinetic energy / section metal temperature / propulsive systems / gas effects / potential energy / /

Organization

National Aeronautics and Space Administration / /

Person

Max Impact / Peter J Ouzts / Min Impact / /

Position

Mode Transition Controller / Nominal Controller / /

Product

Impact / Ram / M-16 / Canard / /

ProgrammingLanguage

Simulink / MATLAB / /

Technology

Simulation / /

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