Axisymmetric Inlet Minimum Weight Design Method by National Aeronautics and Space Adm Nasa

Axisymmetric Inlet Minimum Weight Design Method

National Aeronautics and Space Adm Nasa

42 pages missing pub info (view editions)

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An analytical method for determining the minimum weight design of an axisymmetric supersonic inlet has been developed. The goal of this method development project was to improve the ability to predict the weight of high-speed inlets in conceptual ...

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