发明名称 |
PASSIVE AERODYNAMIC SONIC BOOM SUPPRESSION FOR SUPERSONIC AIRCRAFT |
摘要 |
Sonic boom suppression apparatus for an aircraft (100) including a nose portion (102) having convex upper surfaces and a flat underside, slotted portions on the fuselage (106) or wings (104) of the aircraft, shock cancellation surfaces incorporated in the engine portion (108) of the aircraft, and area/lift distribution tailoring, all of which are preferably used concomitantly.
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申请公布号 |
CA2398528(A1) |
申请公布日期 |
2001.08.16 |
申请号 |
CA20002398528 |
申请日期 |
2000.12.22 |
申请人 |
LOCKHEED MARTIN CORPORATION |
发明人 |
MORGENSTERN, JOHN M.;HARTMANN, TOM |
分类号 |
B64C23/04;B64C30/00;(IPC1-7):B64C30/00 |
主分类号 |
B64C23/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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