Laminar Subsonic, Supersonic, and Transonic Boundary-Layer Flow past a Flat Plate

Autor:	Shourya Prakash Otta, Alric Rothmayer
Rok vydání:	2006
Předmět:	business.industry Aerospace Engineering Laminar flow Geometry Mechanics Computational fluid dynamics Compressible flow Physics::Fluid Dynamics Boundary layer Parasitic drag Incompressible flow Supersonic speed business Transonic Mathematics
Zdroj:	AIAA Journal. 44:102-107
ISSN:	1533-385X 0001-1452
DOI:	10.2514/1.16168
Popis:	A boundary-layer formulation is developed for the low-Mach-number limit. Self-similar low-Mach-number Falkner‐Skan solutions are found for flow past a wedge. From computation of both this low-Mach-number-limit solution and the full compressible boundary-layer equations, it is shown that laminar transonic boundary-layer flow past a constant temperature flat plate may be accurately calculated using the simpler low-Mach-number-limit solution.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::48b5276063b13c259bc62670594a4c98 https://doi.org/10.2514/1.16168 Zobrazit plný text záznamu