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The objective of this study is to estimate the variation of flight performance of a variable sweep wing geometry on the reverse engineered Boeing 2707-100 SST, when compared against the traditional delta wing approach used on supersonic airliner.

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    Date Created
    2021
    Resource Type
  • Text
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    • Partial requirement for: M.S., Arizona State University, 2021
    • Field of study: Aerospace Engineering

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