Configuration was tested in Ames pressurized ballistic range at Mach number of 4.9 to determine interaction of body bow wave with flow field about wing; shadowgraph pictures indicate that body bow wave crosses outer wing panel after first being refracted by interaction with flow field about wing.
Shock-wave patterns on cranked-wing configuration
NASA -- Tech Note
1960
12 pages
Report
English
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Shock-Wave Patterns on a Cranked-Wing Configuration
NTIS | 1960
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