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Rear fuselage transonic flow characteristics for a complete wing-body configuration

Author
COUSTOLS, E1 ; SERAUDIE, A1 ; MIGNOSI, A1
[1] ONERA, 31 055 Toulouse, France
Conference name
Congress of the International Council of the Aeronautical Sciences (20 ; Sorrento, Napoli 1996-09-08)
Source

Journal of aircraft. 1997, Vol 34, Num 3, pp 337-345 ; ref : 13 ref

CODEN
JAIRAM
ISSN
0021-8669
Scientific domain
Aeronautics astronautics; Mechanical engineering; Mechanics acoustics; Transportation
Publisher
American Institute of Aeronautics and Astronautics, Reston, VA
Publication country
United States
Document type
Conference Paper
Language
English
Keyword (fr)
Anémomètre laser Doppler Aéronef Distribution pression Distribution vitesse Ecoulement transsonique Essai soufflerie Essai sur modèle Etude expérimentale Visualisation écoulement
Keyword (en)
Doppler laser anemometer Aircraft Pressure distribution Velocity distribution Transonic flow Wind tunnel test Model test Experimental study Flow visualization
Keyword (es)
Anemómetro laser Doppler Aeronave Distribución presión Distribución velocidad Flujo transónico Ensayo túnel aerodinámico Ensayo sobre modelo Estudio experimental
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D15 Ground, air and sea transportation, marine construction / 001D15J Miscellaneous transportation

Discipline
Building. Public works. Transport. Civil engineering
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
2675361

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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