Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. : II. Mass distributed along the fuselage / Oscar Seidman and A. I. Neihouse.

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Bibliographic Details
Main Author:	Seidman, Oscar
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Neihouse, A. I.
Format:	Government Document Book
Language:	English
Published:	Washington D.C. : National Advisory Committee for Aeronautics, 1937.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 630.
Subjects:	Spin (Aerodynamics) Airplanes > Fuselage. Airplanes > Tail surfaces. Airplanes > Wings. Mass (Physics) Wind tunnel testing. Aerodynamic load.

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Holdings details from PASCAL Offsite
Call Number:	Y 3.N 21/5:6/630
Y 3.N 21/5:6/630	Available Place a Hold