发明名称 Method and apparatus for testing engines
摘要 A scramjet has a cowl, a center structure, and a plurality of wide pylons connecting the cowl to the center structure, with scramjet engines positioned between adjacent pylons. Leading surfaces of adjacent pylons converge to one another to provide side wall compression to air entering the engines. The center structure includes a fore body, a center body and an aft body that, with the pylons, define a basic structure either formed entirely from one piece or several securely connected pieces. A method of testing the scramjet projectile comprises using a gun to accelerate the scramjet projectile to the takeover velocity of the engines.
申请公布号 AU2002345613(A1) 申请公布日期 2003.03.03
申请号 AU20020345613 申请日期 2002.06.10
申请人 ALLIED AEROSPACE INDUSTRIES, INC. 发明人 ROBERT J. BAKOS;RALPH WOELFEL;DEAN MODROUKAS;FLORIN GIRLEA;JOHN I. ENDOS;JASON S. TYLL
分类号 F02C7/04;F02K7/10;F02K9/96;F41B11/00;F42B8/24;F42B15/00;F42B35/00;(IPC1-7):F42B15/10 主分类号 F02C7/04
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