Aerodynamic characteristics of a hypersonic research airplane concept having a 70 swept double-delta wing at mach numbers from 1.50 to 2.86/
| Main Author: | |
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| Corporate Authors: | , , |
| Other Authors: | , |
| Format: | Book |
| Language: | English |
| Published: |
Washington:
National Aeronautics and Space Administration,
1975
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| Series: | NASA technical note
D-8065 |
| Subjects: |