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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
View @ University of Illinois
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Transonic off-design drag and performance of an axisymmetric inlet with 40 percent internal contraction on design
2. Transonic off-design drag and performance of an axisymmetric inlet with 40 percent internal contraction on design

Woollett, Richard R

Keywords:

    Aerodynamic Drag; Aerodynamic Interference; Aerodynamics, Transonic; Air Intakes; Axisymmetric Flow; Drag (Aerodynamics); Engine Inlets; Flow Characteristics; Inlet Flow; Jet Engines; Transonic Flow; Variable Geometry Structures
View @ University of Illinois
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