Wind-tunnel investigation of effects of fuselage cross-sectional shape, fuselage bend, and vertical-tail size on directional characteristics of nonoverlap-type helicopter fuselage models without rotors / James L. Williams.

Saved in:

Bibliographic Details
Main Author:	Williams, James L.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1956.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 3645.
Subjects:	Helicopters > Models. Stability of helicopters. Wind tunnel testing.

PASCAL Offsite

Holdings details from PASCAL Offsite
Call Number:	Y 3.N 21/5:6/3645
Y 3.N 21/5:6/3645	Available Place a Hold