Investigation of effects of geometric dihedral on low-speed static stability and yawing characteristics of an untapered 45 degrees sweptback-wing model of aspect ratio 2.61 / M.J. Queijo and Byron M. Jaquet.

Saved in:

Bibliographic Details
Main Author:	Queijo, M. J.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Jaquet, Byron M.
Other title:	Technical report archive and image library.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 1668.
Subjects:	Airplanes > Wings, Swept-back. Airplanes > Models > Wings. Airplanes > Dihedral wings. Stability of airplanes. Yawing (Aerodynamics) Wind tunnel testing.

PASCAL Offsite

Holdings details from PASCAL Offsite
Call Number:	Y 3.N 21/5:6/1668
Y 3.N 21/5:6/1668	Available Place a Hold