Improved Euler analysis of advanced turboprop propeller flows

Autor:	L. J. Bober, J. M. Barton, O. Yamamoto
Rok vydání:	1986
Předmět:	Turboprop business.industry Mathematical analysis Propeller Mechanics Computational fluid dynamics Compressible flow Euler equations symbols.namesake Inviscid flow Euler's formula symbols Boundary value problem business Mathematics
Zdroj:	22nd Joint Propulsion Conference.
DOI:	10.2514/6.1986-1521
Popis:	An implicit approximate factorization scheme in conjunction with a new boundary treatment was used to compute the inviscid flow field about an advanced high-speed propeller. The method of characteristics was used to apply impermeable boundary conditions. The convergence history of numerical calculations shows substantial decrease in the residual error decay. Euler solutions were computed for SR-3 propeller geometry and the results were compared with the experimental data and previous numerical results.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::2da5e037c8e7d31eb1046319480e434a https://doi.org/10.2514/6.1986-1521 Zobrazit plný text záznamu