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Experimental Investigation of the Aerodynamic Characteristics of an Air-to-Air Missile Employing Cruciform Wings and Tail of Rectangular Plan Form at Mach Numbers of 1.4 and 1.9
| Author: | Mead, Merrill H. |
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| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A52K14 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59483/ |
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