发明名称 Wind-tunnel simulator
摘要 A novel wind-tunnel simulator produces a flow of a gas over a spinning tracer projectile to simulate the flame shape from the tracer projectile as though in actual flight. The wind-tunnel simulator comprises a fixture formed with an opening for receiving the tracer projectile therein spaced from the surface that defines the opening. The fixture is fixed to a motor which is coupled to the projectile for spinning it as though in actual flight. Gas is forced through passageways, formed in the fixture, that communicate with the opening, whereby the gas can flow over the spinning, burning, tracer projectile to simulate in-flight conditions.
申请公布号 US4033185(A) 申请公布日期 1977.07.05
申请号 US19760687577 申请日期 1976.05.18
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE ARMY 发明人 MCNALLY, THOMAS J.;MEHLING, SIGFRIED;PUCHALSKI, WALTER J.
分类号 G01M9/02;(IPC1-7):G01M9/00 主分类号 G01M9/02
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