Data presented for 9 complete models, 20 fuselage shapes, and 3 wing models; author finds it necessary to place considerable reliance on past design experience in proportioning airplane so as to obtain reasonable degree of directional stability.
Estimation of rate of change of yawing moment with sideslip
Nat Advisory Committee Aeronautics -- Tech Note
1938
8 pages
9 Supp sheets, Bibliography
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Estimation of rate of change of yawing moment with sideslip
Engineering Index Backfile | 1938
|Engineering Index Backfile | 1946
|Effects of sideslip on rolling and yawing moments
SLUB | 1932
|