Reinvestigation of theory with special reference to study of manner in which value of so-called critical Mach number for symmetrical Joukowski airfoil varies with angle of attack as well as with thickness ratio of airfoil. (In English.)
On subsonic flow of compressible fluid past symmetrical Joukowski aerofoil
Tokyo Imperial Univ -- Aeronautical Research Inst -- Report
1941
91 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Compressible flow about symmetrical Joukowski profiles
Engineering Index Backfile | 1938
|Compressible flow about symmetrical joukowski profiles
Engineering Index Backfile | 1938
|Compressible flow about symmetrical joukowski profiles
Engineering Index Backfile | 1938
|A generalised type of Joukowski aerofoil
TIBKAT | 1924
|