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A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel
1. A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel

Lawing, Pierce L

Keywords:

    Aerodynamics, Transonic; Ground Simulators; Low Temperature Engineering; Testing; Wind Tunnels
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