Wind-tunnel investigation of effect of sweep on rolling derivatives at angles of attack up to 13 degrees and at high subsonic Mach numbers, including a semiempirical method of estimating the rolling derivatives / James W. Wiggins.

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Bibliographic Details
Main Author:	Wiggins, James W.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington : National Advisory Committee for Aeronautics, [1958]
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 4185.
Subjects:	Airplanes > Wings, Swept-back. Rolling (Aerodynamics) Angle of attack (Aerodynamics) Wind tunnel testing.

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Holdings details from PASCAL Offsite
Call Number:	Y 3.N 21/5:6/4185
Y 3.N 21/5:6/4185	Available Place a Hold