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Optimization of Two-Dimensional Scramjet Inlets

Journal of Aircraft, 1999
The 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 ...
openaire   +4 more sources

Scramjet Operability and RDE Design for RDE Piloted Scramjet

AIAA Scitech 2019 Forum, 2019
Ryan I. Druss   +3 more
openaire   +1 more source

Scramjet Geometry Definition

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.
openaire   +1 more source

Scramjet Engines

Journal of the Society of Mechanical Engineers, 1991
Nobuo CHINZEI, Goro MASUYA
openaire   +1 more source

Scramjet

2018
Walter Bitterlich, Ulrich Lohmann
openaire   +1 more source

Prospects for scramjet engines in reusable launch applications: A review

International Journal of Hydrogen Energy, 2023
Lissen Sam   +2 more
exaly  

Hydrogen fuel in scramjet engines - A brief review

International Journal of Hydrogen Energy, 2020
Gautam Choubey   +2 more
exaly  

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