发明名称 METHOD AND APPARATUS FOR VARIABLE EXHAUST NOZZLE EXIT AREA
摘要 A nozzle effective exit area control system is created with a convergent -- divergent nozzle with a divergent portion of the nozzle having a wall at a predetermined angle of at least 12° from the freestream direction. Disturbance generators are located substantially symmetrically oppositely on the wall to induce flow separation from the wall with the predetermined wall angle inducing flow separation to extend upstream from each disturbance generator substantially to a throat of the nozzle pressurizing the wall and reducing the effective area of the jet flow at the nozzle exit.
申请公布号 CA2754855(C) 申请公布日期 2014.10.07
申请号 CA20112754855 申请日期 2011.10.11
申请人 THE BOEING COMPANY 发明人 WINKLER, CHAD M.;DORGAN, ANDREW J.;WERNER, ERIC L.
分类号 F02K1/06;F02K1/82 主分类号 F02K1/06
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