Results 1 to 10 of about 16,840 (258)
International Journal of Aerospace Engineering, 2023 Liquid oxygen chill-down in a straight horizontal pipe was studied experimentally. The effect of the entrance corner was excluded, and much denser wall temperature sensors along the pipe have been set compared to the present studies.
Lanwei Chen, Jiaqi Zhang
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Investigations on the Influence of the In-Stream Pylon and Strut on the Performance of a Scramjet Combustor [PDF]
The Scientific World Journal, 2014 The influence of the in-stream pylon and strut on the performance of scramjet combustor was experimentally and numerically investigated. The experiments were conducted with a direct-connect supersonic model combustor equipped with multiple cavities.
Hao Ouyang, Weidong Liu, Mingbo Sun
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Direct-Connect Test of Solid Scramjet with Symmetrical Structure
Energies, 2021 The solid scramjet has become one of the most promising engine types. In this paper, we report the first direct-connect test of a solid scramjet with symmetrical structure, carried out using boron-based fuel-rich solid propellant as fuel. During the test,
Pengnian Yang +6 more
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Numerical Investigation of Contact Burning in an Air-Breathing Continuous Rotating Detonation Engine
International Journal of Aerospace Engineering, 2022 Three-dimensional (3D) numerical simulations of a continuous rotating detonation engine are carried out with an unsteady Reynolds-averaged Navier-Stokes solver.
Dapeng Xiong +7 more
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International Journal of Aerospace Engineering, 2022 Liquid oxygen chill-down in a vertical exit-contracted pipe was investigated experimentally. The wall temperatures were recorded in detail to describe the filling and chill-down process of the experimental section.
Jiaqi Zhang, Ke Wang, Lanwei Chen
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Experimental Study of the Formation and Evolution of Gas Jets in Supersonic Combustion Chambers
Applied Sciences, 2023 A simple and efficient flow field visualization method (based on shadow imaging) was applied in a direct-connect test to explore the influence of the momentum flux ratio and the jet angle on the formation and evolution of nitrogen jets in supersonic ...
Yifan Duan +6 more
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Design method of supercritical hydrocarbon fuel injection for a scramjet
Advances in Aerodynamics, 2022 Both the fuel transfer control scheme and the knowledge of fuel temperature and pressure values before injection are important to a scramjet engine.
Lei Zhang +3 more
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Aerospace, 2022 The ethylene-fueled flameholding characteristics of a cavity-based scramjet combustor are experimentally and numerically investigated. The test facility used the air heater, which heats air from room temperature to total temperature 1477 K.
Zhonghao He +5 more
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AIP Advances, 2022 This study investigates the characteristics of a turbulent boundary layer in a curved circular pipe under an inflow of Ma = 3.0. The pipe consisted of a straight part and a curved part with a turning angle of 36° and a radius of curvature, γ = R/Rc, of γ
Chang-Hai Liang +8 more
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International Journal of Aerospace Engineering, 2021 An axisymmetric model scramjet assisted with cavity flameholder is numerically investigated. Three-dimensional Reynolds-averaged Navier-Stokes simulation is carried out to reveal the fuel mixing and combustion characteristics. The simulation results show
Guangwei Ma +6 more
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