Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
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| Main Authors: | , |
|---|---|
| Corporate Author: | |
| Format: | Government Document Electronic eBook |
| Language: | English |
| Published: |
[Washington, D.C.] :
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
December 1980.
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| Series: | NASA technical paper ;
1767. |
| Subjects: | |
| Online Access: | CONNECT |
