Application of static integrated skeletal reduction and tabulation of dynamic adaptive chemistry in the combustion simulation of ethylene-fueled scramjet combustor. [PDF]
RSC AdvLi Z, Liu J, Wang J.
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Computational modeling of the rectangular non-aligned multi-injector for efficient fuel mixing in a supersonic combustion chamber. [PDF]
Sci RepZhang P, Li Z, Abdollahi SA.
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A Study on Design of S-Duct Structures and Air Intake for Small Aircraft Applied to High Strength Carbon-Epoxy Composite Materials. [PDF]
Materials (Basel), 2022 Lim S, Choi W, Park H.
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The Reinforcing Effect of Cluster Materials in the Combustion of Hydrocarbon Fuels. [PDF]
Int J Mol SciWang X +5 more
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Aerodynamic problems in scramjet.
Journal of the Japan Society for Aeronautical and Space Sciences, 1990 CNINZEI, Nobuo, MASUYA, Goro
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Influence of the non-equal aligned nozzles for fuel injection inside the supersonic combustion chamber. [PDF]
Sci RepFan Z +7 more
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Numerical study on the start and unstart phenomena in a scramjet inlet-isolator model. [PDF]
PLoS One, 2019 Lee J, Kang SH.
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US hypersonics initiatives require accelerated efforts of the materials research community. [PDF]
MRS Bull, 2021 europepmc +1 more source
Calculation of Scramjet Performance
Calculation of Scramjet PerformanceIn this paper, the performance of an airframe-integrated scramjet engine is calculated using a quasi-one-dimensional model. The forebody of the airframe is approximated as a cone. Experimental data correlations are used to estimate pressure recovery and capture area of the inlet.
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A High-Performance Ultraviolet Optical Sensing System for Rotating Detonation Extreme Combustion. [PDF]
Sensors (Basel)Dai W +7 more
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