An integrated and/or modular high-speed aircraft (1200) and method of design. The aircraft (1200) can have a supersonic or near-sonic cruise Mach number. In one embodiment, the aircraft can include an aft body (1214) integrated with a delta wing (1204) and a rearwardly tapering fuselage (1202) to define a smooth forward-to-rear area distribution. An engine (1216), inlet, and exhaust nozzle can be integrated into the aft body to be at least partially hidden behind the wing (1204).
申请公布号
WO02057135(A1)
申请公布日期
2002.07.25
申请号
WO2001US02368
申请日期
2001.01.19
申请人
THE BOEING COMPANY;NELSON, CHESTER, P.;SEIDEL, GERHARD, E.