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Propulsion Wind Tunnel Facility : ウィキペディア英語版
Propulsion Wind Tunnel Facility

The Propulsion Wind Tunnel Facility, located at Arnold Engineering Development Complex, Arnold Air Force Base, Tennessee, holds three wind tunnels: the 16-foot transonic (16T), 16-foot supersonic (16S), and the aerodynamic 4-foot transonic (4T) tunnels. The facility is devoted to aerodynamic and propulsion integration testing of large-scale aircraft models. The tunnels are powered by a large compressor plant which allows the wind tunnels to run for extended periods of time.〔(【引用サイトリンク】title=Factsheets : PROPULSION WIND TUNNEL FACILITY )〕 The test unit is owned by the United States Air Force and operated by Aerospace Testing Alliance.
== Propulsion Wind Tunnel 16T ==
16T is a transonic wind tunnel that can be configured for Mach numbers from 0.05 to 1.60. It is primarily used to test aerodynamics, propulsion integration, and weapons integration test capabilities that are needed for accurate prediction of flight system performance. The test section 16-foot-square, 40-foot long test section can simulate unit Reynolds numbers from approximately 0.03 to 7.3 million per foot or altitude conditions from sea level to 76,000 feet. The tunnel can also test air-breathing engines and rockets through the use of a scavenging system to remove exhaust from the flow stream.〔(【引用サイトリンク】title=Factsheets : PROPULSION WIND TUNNEL 16T )

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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