Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps - Trailing-edge Flaps Deflected
1950-12-13
Miscellaneous
No indication
English
Engineering Index Backfile | 1937
|Emerald Group Publishing | 1937
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