An analytical design procedure for the determination of effective leading edge extensions on thick delta wings

An analytical design procedure for the determination of effective leading edge extensions on thick delta wings [microform] / by Farhad Ghaffari and Sushil K. Chaturvedi, principal investigator ; prepared for the National Aeronautics and Space Administration, Langley Research Center.

Aerodynamic coefficients; Delta wings; Leading edges; Lift; Aircraft performance; Aspect ratio; Supersonic aircraft.

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Bibliographic Details
Main Author:	Ghaffari, Farhad
Corporate Authors:	Langley Research Center, Old Dominion University. Research Foundation, Old Dominion University. Department of Mechanical Engineering and Mechanics, United States. National Aeronautics and Space Administration
Other Authors:	Chaturvedi, Sushil K.
Format:	Government Document Microfilm Book
Language:	English
Published:	Norfolk, VA : Hampton, Va. : Old Dominion University ; The Center, [1984]
Series:	NASA contractor report ; NASA CR-175395.
Subjects:	Airplanes > Wings, Triangular. Leading edges (Aerodynamics) > Testing.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:175395
NAS 1.26:175395	Restricted Place a Hold