Study on integrated control for supersonic inlet and turbofan engine model
Sign Up to like & getrecommendations! Published in 2020 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/0954410020944068
Abstract: Considering the supersonic inlet model with normal shock position feedback, the integrated control method of inlet and turbofan engine is studied. The integrated model includes the supersonic inlet model and the component level model of… read more here.
Keywords: inlet; control; engine; supersonic inlet ... See more keywords
Experimental and numerical investigation of a supersonic inlet with double S-bend diffuser
Sign Up to like & getrecommendations! Published in 2021 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/0954410020983981
Abstract: Design of a supersonic inlet with double S-bend diffuser was developed. Numerical simulation and wind tunnel experiment were carried out to investigate the aerodynamic performance and variable geometric rules of the inlet. The result indicates… read more here.
Keywords: bend; bend diffuser; supersonic inlet; double bend ... See more keywords
Effect of Side Gust on Performance of External Compression Supersonic Inlet
Sign Up to like & getrecommendations! Published in 2019 at "Journal of Aircraft"
DOI: 10.2514/1.c035093
Abstract: This Paper reports a computational investigation on the effects of side gust on the performance of a double-cone external compression supersonic inlet at Mach 1.8. The supersonic inlet geometry com... read more here.
Keywords: external compression; compression supersonic; side gust; inlet ... See more keywords
Flow Asymmetry in a Y-Shaped Diverterless Supersonic Inlet: A Novel Finding
Sign Up to like & getrecommendations! Published in 2020 at "AIAA Journal"
DOI: 10.2514/1.j059006
Abstract: Extensive wind-tunnel tests were performed on a Y-shaped diverterless supersonic inlet (DSI). All tests were conducted at a free stream Mach number of M∞=1.65, the design Mach number for this inlet... read more here.
Keywords: inlet; flow asymmetry; shaped diverterless; diverterless supersonic ... See more keywords
Linear and Nonlinear Flow Analysis of Elements of a Supersonic Inlet
Sign Up to like & getrecommendations! Published in 2021 at "AIAA Journal"
DOI: 10.2514/1.j060591
Abstract: Boundary layer development in a supersonic inlet is studied, focusing on the flow over the compression ramp and the ramp–isolator junction. Two designs of the junction, a backward-facing step (BFS)... read more here.
Keywords: flow analysis; linear nonlinear; nonlinear flow; inlet ... See more keywords