Influence of sideslip on double delta wing aerodynamics
- Autor
- GRISMER, D. S1 ; NELSONR. C2 ; ELY, W. L3
[1] Wright-Patterson AFB, Wright lab., United States
[2] Univ. Notre Dame, Notre Dame IN 46556, United States
[3] McDonnell Aircraft Co., St Louis MI 63166, United States - Fuente
Journal of aircraft. 1995, Vol 32, Num 2, pp 451-453 ; ref : 7 ref
- CODEN
- JAIRAM
- ISSN
- 0021-8669
- Campo Científico
- Aeronautics astronautics; Mechanical engineering; Mechanics acoustics; Transportation
- Editor
- American Institute of Aeronautics and Astronautics, Reston, VA
- País de la publicación
- United States
- Tipo de documento
- Article
- Idioma
- English
- Palabra clave (fr)
- Aile delta Aérodynamique Distribution pression Dérapage Etude expérimentale Forme géométrique Tourbillon Angle dérapage
- Palabra clave (in)
- Delta wing Aerodynamics Pressure distribution Side slip Experimental study Geometrical shape Vortices
- Palabra clave (es)
- Ala delta Distribución presión Derrapaje Forma geométrica
- Clasificación
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G85 Applied fluid mechanics / 001B40G85B Aerodynamics
- Disciplina
- Physics : fluid mechanics
- Procedencia
- Inist-CNRS
- Base de datos
- PASCAL
- Identificador INIST
- 3494074
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
10.2514/3.46740 
https://dx.doi.org/10.2514/3.46740
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