WebApr 28, 2004 · For stealth aircraft, it would seem easier for side intakes to wrap around an internal weapons bay. The Boeing JSF had a chin intake, but had to resort to shrouding the engine fan instead of curving the … Webinlet, @ = 2 x 55 degrees for the twin-scoop inlets, and 8 = 360 degrees for the annular inlet. Five basic inlet configurations were selected for design and experimental evaluation with an advanced eight-bladed 45 degree swept (SR-3) propfan (Reference 2). They were two single-scoop, or chin inlet, configurations
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WebChin inlet Supersonic combustor Supersonic combustor Supersonic diffuser Subsonic diffuser Subsonic combustor Combustor Subsonic diffuser Solid propellant Boost propellant Figure 1. Candidate engine cycles for hypersonic vehicles. combined cycle engines, such as the Dcr (Fig. 1f) and turbo-ramjet, offer design features that enhance engine WebMar 1, 2024 · The S-shaped inlet of the modern military aircraft propulsion system suffers from severe inlet distortion during flight maneuvering. The complex distorted flow field is generally decomposed into total pressure and swirl distortion, both of which could substantially degrade the performance and stability of an aero-engine. roman rabl
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