Conical, noncircular, second-order, potential theory of supersonic flow

Autor:	L. Devan
Rok vydání:	1984
Předmět:	business.industry Angle of attack Computation Numerical analysis Mathematical analysis Finite difference Aerospace Engineering Geometry Computational fluid dynamics Symmetry (physics) symbols.namesake Euler's formula symbols business Linear equation Mathematics
Zdroj:	AIAA Journal. 22:618-623
ISSN:	1533-385X 0001-1452
DOI:	10.2514/3.8646
Popis:	This is the first application of the Van Dyke iterative model to noncircular cross-sectional bodies. Two finite difference numerical methods are presented to solve the first and second-order linear equations. Excellent comparisons with Euler model computations are obtained for cones at angle of attack and sideslip. Computation times for flows with planar symmetry are 1.5-3.0 s on a CDC 6400 computer.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::ab98c097d2d6bf474e3ad59b719758b5 https://doi.org/10.2514/3.8646 Zobrazit plný text záznamu