Trailing edge flow conditions as a factor in airfoil design /

Bibliographic Details
Main Author:	Ormsbee, A. I.
Corporate Authors:	University of Illinois at Urbana-Champaign. Aeronautical and Astronautical Engineering Department, United States. National Aeronautics and Space Administration
Other Authors:	Maughmer, Mark D.
Format:	Government Document Book
Language:	English
Published:	Urbana, Ill. : [Washington, DC] : Aeronautical and Astronautical Engineering Dept., University of Illinois ; [National Aeronautics and Space Administration], [1984]
Series:	Technical report (University of Illinois at Urbana-Champaign. Aeronautical and Astronautical Engineering Department) ; AAE 84-1. NASA contractor report ; NASA CR-173294.
Subjects:	Aerofoils > Design and construction. Trailing edges (Aerodynamics) Aircraft design. Airfoils. Potential flow. Pressure gradients. Trailing edges.
Online Access:	https://purl.fdlp.gov/GPO/LPS86754

Description
Item Description:	Microform.
Physical Description:	1 volume 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.