Effect of chordwise location of maximum thickness on the supersonic wave drag of sweptback wings
1948-03-01
Miscellaneous
No indication
English
Effect of chordwise location of maximum thickness on supersonic wage drag of sweptback wings
Engineering Index Backfile | 1948
|Engineering Index Backfile | 1948
|Supersonic wave drag of sweptback tapered wings at zero lift
Engineering Index Backfile | 1947
|Theoretical supersonic wave drag of untapered sweptback and rectangular wings at zero lift
Engineering Index Backfile | 1947
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