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Counterflow drag reduction by supersonic jet for a blunt body in hypersonic flow

Author
VENUKUMAR, Balla1 ; JAGADEESH, G1 ; REDDY, K. P. J1
[1] Department of Aerospace Engineering, Indian Institute of Science, Bangalore-560012, India
Source

Physics of fluids (1994). 2006, Vol 18, Num 11 ; 118104.1-118104.4 ; ref : 9 ref

CODEN
PHFLE6
ISSN
1070-6631
Scientific domain
Mechanics acoustics
Publisher
American Institute of Physics, Melville, NY
Publication country
United States
Document type
Article
Language
English
Keyword (fr)
Aérodynamique Corps émoussé Ecoulement contre courant Ecoulement hypersonique Etude expérimentale Jet supersonique Réduction traînée Strioscopie Tube choc Visualisation écoulement
Keyword (en)
Aerodynamics Blunt body Countercurrent flow Hypersonic flow Experimental study Supersonic jet Drag reduction Schlieren method Shock tubes Flow visualization
Keyword (es)
Cuerpo embotado Flujo contra corriente Chorro supersónico
Classification
Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G80 Instrumentation for fluid dynamics

Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G85 Applied fluid mechanics / 001B40G85B Aerodynamics

Pacs
4780 Instrumentation for fluid dynamics

Discipline
Physics : fluid mechanics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
18367375

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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