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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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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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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Simulation at Mach 2 flow of ethylene/air reacting mixture within a cavity flame holder. [PDF]
HeliyonChapman Z, Peterson D, Doom J.
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Aerodynamic problems in scramjet.
Journal of the Japan Society for Aeronautical and Space Sciences, 1990 Nobuo CNINZEI, Goro MASUYA
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Usage of double injector for efficient mixing of the fuel behind the ramp injector at supersonic combustion chamber. [PDF]
Sci RepOmar I +9 more
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Novel post-processing methods for infrared measurements on porous surfaces. [PDF]
Sci RepHärter J, Lamanna G, Poser R.
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Multi-Functional Properties of MWCNT/PVA Buckypapers Fabricated by Vacuum Filtration Combined with Hot Press: Thermal, Electrical and Electromagnetic Shielding. [PDF]
Nanomaterials (Basel), 2020 Cao L +6 more
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