An analytical design procedure for the determination of effective leading edge extensions on thick delta wings
By: by Farhad Ghaffari and Sushil K. Chaturvedi, principal investigator ; prepared for the National Aeronautics and Space Administration, Langley Research Center
Contributors: Chaturvedi, Sushil K; Langley Research Center; Old Dominion University. Research Foundation; Old Dominion University. Dept. of Mechanical Engineering and Mechanics
Series: NASA-CR -- 175395; NASA contractor report -- 175395
Publisher: The Center
Published: 1984
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Wings, Triangular; Leading edges (Aerodynamics) -- Testing
Notes: "Final report for the period ending January 15, 1983."

"Submitted by the Old Dominion University Research Foundation."

"Department of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University."

"February 1984."

"Research grant NAS-1-17099, task authorization no. 26."

"N84-19284"--Microfiche header

Includes bibliographical references

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1984]. 1 microfiche ; 11 x 15 cm