Determination of the optimal contour of a supersonic jet engine outlet by the direct method
- Author
- AUKIN, M. K; TAGIROV, R. K
- Source
Fluid dynamics. 1998, Vol 33, Num 1, pp 140-146 ; ref : 10 ref
- ISSN
- 0015-4628
- Scientific domain
- Mechanics acoustics
- Publisher
- Consultants Bureau, New York, NY
- Publication country
- United States
- Document type
- Article
- Language
- English
- Keyword (fr)
- Aéronef Conception optimale Echappement Forme géométrique Optimisation Propulseur réaction Simulation numérique Tuyère Vol supersonique
- Keyword (en)
- Aircraft Optimal design Exhaust Geometrical shape Optimization Jet engine Numerical simulation Tuyere Supersonic flight
- Keyword (es)
- Aeronave Concepción optimal Escape Forma geométrica Optimización Propulsor reacción Simulación numérica Tobera Vuelo supersónico
- Classification
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D15 Ground, air and sea transportation, marine construction / 001D15I Air transportation and traffic
- Discipline
- Building. Public works. Transport. Civil engineering
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 1606907
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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DOI
10.1007/BF02698172 
https://dx.doi.org/10.1007/BF02698172
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