Study of potential aerodynamic benefits from spanwise blowing at wingtip.

Bibliographic Details

Main Author:	Mineck, Raymond E.
Corporate Author:	Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [1995]
Series:	NASA technical paper ; 3515.
Subjects:	Aerodynamic drag. Aerodynamics. Commercial aircraft. Lift. Navier-Stokes equation. Spanwise blowing. Subsonic speed. Swept wings. Wind tunnel tests.