Trailing edge flow conditions as a factor in airfoil design
By: by A. I. Ormsbee and Mark D. Maughmer.
Contributors: Maughmer, Mark D.; University of Illinois at Urbana-Champaign. Aeronautical and Astronautical Engineering Dept.; United States. National Aeronautics and Space Administration.
Series: NASA CR -- 173294.; Technical report -- AAE 84-1.; Technical report (University of Illinois at Urbana-Champaign. Aeronautical and Astronautical Engineering Dept.) -- AAE 84-1.; NASA contractor report -- NASA CR-173294.
Publisher: Aeronautical and Astronautical Engineering Dept., University of Illinois; National Aeronautics and Space Administration
Published: 1984
Place of publication: Urbana, Ill; [Washington, DC
Language: eng
Format: Microform
Subjects: Aerofoils -- Design and construction.; Trailing edges (Aerodynamics); Aircraft design.; Airfoils.; Potential flow.; Pressure gradients.; Trailing edges.
Notes: Also available via Internet from the NTRS web site. Address as of 10/10/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19840009072%5F1984009072.pdf  ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1984. 2 microfiches.