Methods developed permit computation of lift and drag of delta wings for large family of plan forms and thickness distributions; delta wing properly designed can be used to reduce minimum drag to roughly two thirds that of low aspect ratio rectangular wing, without impairing its lifting efficiency. Before Inst Aeronautical Sciences.
Aerodynamic performance of Delta wings at supersonic speeds
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 14 , n 10
1947
12 pages
Article (Journal)
English
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Aerodynamic performance of Delta wings at supersonic speeds
Engineering Index Backfile | 1948
|Aerodynamic performance of Delta wings at supersonic speeds
Engineering Index Backfile | 1948
|Aerodynamic characteristics of rectangular wings at supersonic speeds
Engineering Index Backfile | 1947
|