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Influence of the jet pressure ratio on the performance of an AGARD single flow afterbody in the 0.60-0.95 Mach range
Influence of the jet pressure ratio on the performance of an AGARD single flow afterbody in the 0.60-0.95 Mach range
1975
B. Mechin
Janet M. B. Hardy
Keywords:
Atmospheric sciences
Subsonic and transonic wind tunnel
Overall pressure ratio
Hypersonic wind tunnel
Transonic
Mach number
Aerospace engineering
Boundary layer
Physics
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