Effects of angle of attack and ventral fin on transonic flutter characteristics of an arrow-wing configuration /

Effects of angle of attack and ventral fin on transonic flutter characteristics of an arrow-wing configuration /

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Bibliographic Details
Main Author:	Doggett, Robert V
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Branch, Langley Research Center
Other Authors:	Ricketts, Rodney H
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service], 1980
Series:	NASA technical memorandum 81914 NASA technical memorandum 81914
Subjects:	Aerodynamics, Transonic Flutter (Aerodynamics) Oscillating wings (Aerodynamics)
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Stanford University

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Call Number:	ISIL:US-CST MARCIVE NAS 1.15:81914 NASA TM 81914