Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
By: by Ken Craig.
Contributors: Joint Institute for Aeronautics and Acoustics.; Ames Research Center.
Series: JIAA TR -- 104.; NASA CR -- 187979.; NASA contractor report -- NASA CR-187979.
Publisher: Stanford University, Dept. of Aeronautics and Astronautics; National Aeronautics and Space Administration, Ames Research Center
Published: 1991
Place of publication: Stanford, Calif; [Moffett Field, Calif.?]
Language: eng
Format: Microform
Number of pages: 37
Subjects: Unsteady flow (Aerodynamics); Airplanes -- Control surfaces.; Delta wing airplanes.; Delta wings.; Equilibrium flow.; Flow distribution.; Grid generation (Mathematics); Turbulence models.; Upper surface blowing.; Wing profiles.
Notes: Cover title.

At head of title: Joint Institute for Aeronautics and Acoustics.

"September 1991."

Includes bibliographical references (p. 19-20).

Also available via Internet from the NASA Technical Report Server web site. Address as of 4/20/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19920001772%5F1992001772.pdf  ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1991. 1 microfiche.