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Northrop Switchblade : ウィキペディア英語版 | Northrop Switchblade
The Northrop "Switchblade" is a concept fighter jet which is a potential development of a utility patent filed by Grumman () in November 1999. ==Design and development==
The wings are attached to the fuselage (body) at a pivot point toward the rear of the aircraft. With the wings fully swept aft the aircraft can slow to drop precision weapons or land on short unimproved runways. Swept forward twenty degrees and the aircraft takes advantage of the maneuverability that forward-swept wings offer becoming a highly agile air combat platform. Swept fully forward the wings become flush with the aircraft with the trailing edge becoming the leading edge, forming a highly swept 75-degree stealthy delta ideal for high-speed Mach 3 ''exits''. Or, as it is stated in the U.S. Patent 5,984231 abstract, "the aforementioned apparatus may be used in a method to configure the aircraft for flight in a desired flight regime".
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Northrop Switchblade」の詳細全文を読む
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