Results of measurements made at fairly large Reynolds Number in California Institute of Technology (GALCIT) 10-ft wind tunnel on two highly tapered wings; force measurements; lines of flow separation; distribution of lift.
On stalling of highly tapered wings
J Aeronautical Sciences
Journal of Aeronautical Sciences ; 3 , n 5
1936
6 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1936
|Engineering Index Backfile | 1936
|Engineering Index Backfile | 1935
|Emerald Group Publishing | 1937
Design charts relating to stalling of tapered wings
Engineering Index Backfile | 1940
|