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.
Computer-aided design analysis of hypersonic aircraft air intake geometry
Russian Aeronautics (Iz VUZ) ; 56 , 3 ; 274-279
2013-07-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Computer-aided design analysis of hypersonic aircraft air intake geometry
Online Contents | 2013
|NTRS | 1990
|NTIS | 1990
|Computer aided aircraft structural design
AIAA | 1968
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