The Calculation of Two-Dimensional Transonic Flow over Aerofoils Including Boundary Layer and Wake Effects Canadair Limited

Format:

Conference/Event

Author/Creator:

Bansod, Prakash, author.

Conference Name:

Business Aircraft Meeting and Exposition (1983-04-12 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1983

Summary:

A brief description is given of the development of a weak interaction method for calculating transonic flows over aerofoils. Viscous effects are introduced by changing the boundary conditions on the aerofoil surface and wake. The wake thickness and curvature are taken into account. The method is evaluated against experimental data for eight aerofoils with sharp and thick trailing edges. Comparisons between experiment and theory are presented for turbulent boundary layer parameters, pressure distribution and drag

Notes:

Vendor supplied data

Publisher Number:

830708

Access Restriction:

Restricted for use by site license