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About Drag Characteristics Obtained From Several Configurations of the Modified X-15-2 Airplane up to ...
Mach 3.8 and 4.9 was about 0.006 at a lift coefficient of 0. 1 and 0 .. a, coso. D Il Z. The base pressure coefficients were determined from the following
Detailed Information
Author: | Lawrence C. Montoya |
---|---|
Publication Year: | 2002 |
Pages: | 30 |
Language: | English |
File Size: | 1.14 |
Format: | |
Price: | FREE |
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