Theoretical results for the initial lift-curve slope of straight-tapered wings, based on the linearized equations of inviscid motion, have been evaluated and are presented in the form of graphs.
Lift-Curve Slope at Subsonic and Supersonic Speeds
Graphical Presentation of Theoretical Results for Straight-Tapered Wings
Aircraft Engineering and Aerospace Technology ; 26 , 8 ; 244-257
1954-08-01
14 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Lift-curve slope at subsonic and supersonic speeds
Engineering Index Backfile | 1954
|Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds
Engineering Index Backfile | 1954
|Lift developed on unrestrained rectangular wings entering gusts at subsonic and supersonic speeds
Engineering Index Backfile | 1953
|