发明名称 Boundary layer control diffuser for a wind tunnel or the like
摘要 A wind tunnel having a test section and a fan section, interconnected by two passageways to form a recirculating air flow through said sections. There is a diffuser immediately downstream of the test section, and a second diffuser immediately downstream of the fan section. Each diffuser has an intermediate flow section where the side wall extends radially outwardly in a downstream direction at a relatively sharp angle. At the upstream end of the intermediate section there is a peripheral suction slot to draw in boundary layer air, and a by-pass passageway to discharge the air tangentially in a downstream location of the diffuser. This enables a substantial reduction in air velocity in a relatively short axial length.
申请公布号 US5099685(A) 申请公布日期 1992.03.31
申请号 US19900565802 申请日期 1990.08.09
申请人 THE BOEING COMPANY 发明人 MCLEAN, JAMES D.;SULLIVAN, PETER P.
分类号 G01M9/04 主分类号 G01M9/04
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