Experimental investigation of effect of vertical-tail size and length and of fuselage shape and length on static lateral stability characteristics of model with 45° sweptback wing and tail surfaces.
Experimental investigation of effect of vertical-tail size and length and of fuselage shape and length on static lateral stability characteristics of model with 45° sweptback wing and tail surfaces
Nat Advisory Committee Aeronautics -- Tech Note
1950
59 pages
Illustrations, Diagrams, Charts, Tables
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1951
|