Integration of the supersonic kernel function
- Author
- VAN ZYL, L. H
CSIR, AEROTEK, Pretoria 0001, South Africa - Source
Journal of aircraft. 1994, Vol 31, Num 6, pp 1433-1435 ; ref : 3 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
- Article
- Language
- English
- Keyword (fr)
- Aérodynamique Distribution pression Ecoulement supersonique Fonction noyau Méthode panneau Théorie surface portante
- Keyword (en)
- Aerodynamics Pressure distribution Supersonic flow Kernel function Panel method Lifting surface theory
- Keyword (es)
- Distribución presión Función núcleo Método panel Teoría superficie portante
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G85 Applied fluid mechanics / 001B40G85B Aerodynamics
- Discipline
- Physics : fluid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 3492258
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
10.2514/3.46675 
https://dx.doi.org/10.2514/3.46675
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