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Optimization of Two-Dimensional Scramjet Inlets
Journal of Aircraft, 1999The classical optimization of two-dimensional supersonic inlets for maximum total pressure recovery is extended to two-dimensional scramjet inlets. The result that optimal supersonic inlets have shock waves of equal strength is often applied to scramjets, However the typical flow turning constraint required for scramjets, along with the lack of a ...
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Scramjet Operability and RDE Design for RDE Piloted Scramjet
AIAA Scitech 2019 Forum, 2019Ryan I. Druss +3 more
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1991
This appendix presents the exact geometry used for the scramjet calculations of chapter 8. Figure B.1 gives the geometry of the 2-D scramjet. Figure B.2 gives an x - y slice of the geometry of the 3-D scramjet at z = 0, Fig. B.3 gives an x - y slice of the geometry of the 3-D scramjet at z = 1.
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This appendix presents the exact geometry used for the scramjet calculations of chapter 8. Figure B.1 gives the geometry of the 2-D scramjet. Figure B.2 gives an x - y slice of the geometry of the 3-D scramjet at z = 0, Fig. B.3 gives an x - y slice of the geometry of the 3-D scramjet at z = 1.
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Journal of the Society of Mechanical Engineers, 1991
Nobuo CHINZEI, Goro MASUYA
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Nobuo CHINZEI, Goro MASUYA
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Prospects for scramjet engines in reusable launch applications: A review
International Journal of Hydrogen Energy, 2023Lissen Sam +2 more
exaly
Hydrogen fuel in scramjet engines - A brief review
International Journal of Hydrogen Energy, 2020Gautam Choubey +2 more
exaly

