Computer-aided design analysis of hypersonic aircraft air intake geometry

Computer-aided design analysis of hypersonic aircraft air intake geometry

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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Veröffentlicht in:Russian aeronautics 2013-07, Vol.56 (3), p.274-279
1. Verfasser: Gainutdinov, V. G.
Format: Artikel
Sprache:eng
Schlagworte:
Air intakes
Aircraft and Rocket Engine Design and Development
Automotive Engineering
Engineering
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Beschreibung
Zusammenfassung: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.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799813030094