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This thesis examines the modeling, analysis, and control system design issues for scramjet powered hypersonic vehicles. A nonlinear three degrees of freedom longitudinal model which includes aero-propulsion-elasticity effects was used for all analysis. This model is based upon classical compressible flow and Euler-Bernouli structural concepts.

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    Date Created
    2010
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  • Text
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    • Partial requirement for: M.S., Arizona State University, 2010
      Note type
      thesis
    • Includes bibliographical references (p. 152-
    • Field of study: Electrical engineering

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    by Akshay Shashikumar Korad

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