NASA Technical Reports Server (NASA) · 1971 · 12 citations · 2 references
Open access
EngineeringAerospace EngineeringPhysicsAerodynamicsFluid DynamicsTunnel EngineeringExperimental AerodynamicsWind-tunnel TestingExperimental Transonic Wind TunnelsHigh-mach-number AerodynamicsMach NumberMach Number Effects
Measurements of sonic boom pressure distribution of bodies of revolution at Mach 2.96, 3.83, and 4.63 in Unitary Plan wind tunnel
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