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Drag Characteristics Obtained From Several Configurations of the Modified X-15-2 Airplane up to ... PDF

30 Pages·2002·1.14 MB·English
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by Lawrence C. Montoya| 2002| 30 pages| 1.14| English

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

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Author:Lawrence C. Montoya
Publication Year:2002
Pages:30
Language:English
File Size:1.14
Format:PDF
Price:FREE
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