Abstract In this paper, a numerical algorithm for design analysis and optimization of hypersonic aircraft air intake geometry is presented. The analysis data show that the algorithms being proposed are sufficiently accurate for preliminary analysis and optimization of design parameters.


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    Title :

    Computer-aided design analysis of hypersonic aircraft air intake geometry


    Contributors:

    Published in:

    Publication date :

    2013-07-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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