作者: Chester P. Nelson
DOI:
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摘要: An integrated and modular high-speed aircraft (200) method of design manufacture. The can have a supersonic or near-sonic cruise Mach number. In one embodiment, the include an aft body with delta wing (204) rearwardly-tapering fuselage (202) to define smooth forward-to-rear area distribution. A propulsion system (206), including engine (216), inlet (220), exhaust nozzle (222) be into at least partially hidden behind (204). entrance positioned beneath (204), exit above S-shaped duct (221) deliver air aft-mounted engine.