Method of calculating the compressible flow round an aerofoil or a cascade up to the shockfree transonic range

Autor:	Geneviève Coulmy, Thoai-Sum Luu
Rok vydání:	1977
Předmět:	Physics Airfoil General Computer Science Plane (geometry) Astrophysics::High Energy Astrophysical Phenomena General Engineering Mechanics Compressible flow Physics::Fluid Dynamics Classical mechanics Flow (mathematics) Cascade Range (statistics) Gravitational singularity Transonic
Zdroj:	Computers & Fluids. 5:261-275
ISSN:	0045-7930
DOI:	10.1016/0045-7930(77)90011-1
Popis:	A computational scheme based on the singularities distribution is developed to treat the transonic potential plane flow.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::e674d232a6e13da7c0bdb8e7aa7f0278 https://doi.org/10.1016/0045-7930(77)90011-1 Zobrazit plný text záznamu