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Von Karman Gas Dynamics Facility : ウィキペディア英語版 | Von Karman Gas Dynamics Facility
The von Karman Gas Dynamics Facility at Arnold Engineering Development Complex, Arnold Air Force Base, Tennessee, provide aerothermal ground test simulations of hypersonic flight over a wide range of velocities and pressure altitudes. The facility consists of three Hypersonic wind tunnels: Tunnel A, B, and C. The wind tunnels can be run for several hours at a time thanks to a 92,500 horsepower air compressor plant system.〔(【引用サイトリンク】title=Factsheets : THE VON KARMAN GAS DYNAMICS FACILITY WIND TUNNELS )〕 The test unit is owned by the United States Air Force and operated by Aerospace Testing Alliance. == Tunnel A == Tunnel A is a 40-inch squared, continuous, closed-circuit, variable density, supersonic wind tunnel with a Mach number range of 1.5 to 5.5 with a maximum temperature of 290 degress Fahrenheit. Devoted primarily to explorations of aerodynamic design, Tunnel A's unique feature is its computer controlled continuous-curvature nozzle that can vary the tunnel's Mach number.
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