Supersedes NACA -- Tech Note 2168 indexed in Engineering Index 1950 p 54. (25¢)
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
NACA -- Report
1951
29 pages
Illus, Diagrs, Charts
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1951
|