Experimental Investigation on the Transpiration Cooling Characteristics of Sintered Wire Mesh in Plain Weave. [PDF]
Micromachines (Basel), 2022 Peng Y, Xu G, Luo X, He J, Liu D.
europepmc +1 more source
Advanced ramjet concepts program [PDF]
Uniquely advantageous features, on both the performance and weight sides of the ledger, can be achieved through synergistic design integration of airbreathing and rocket technologies in the development of advanced orbital space transport propulsion ...
Leingang, J. L.
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Usage of serpentine injector for hydrogen mixing at combustion chamber of scramjet engine via a computational study. [PDF]
Sci RepMir A +7 more
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Experimental Study on the Unsteady Spray Combustion Process of a Liquid Oxygen/Methane Swirl Coaxial Injector. [PDF]
ACS Omega, 2021 Cao P, Bai X, Li Q, Cheng P, Li Z.
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A New Hypersonic Wind Tunnel Force Measurement System to Reduce Additional Bending Moment and Avoid Time-Varying Stiffness. [PDF]
Sensors (Basel), 2022 Li S, Liu Z, Zhao F, Gao H.
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A parametric experimental investigation of a scramjet nozzle at Mach 6 with Freon and argon or air used for exhaust simulation [PDF]
A parametric experimental investigation of a scramjet nozzle was conducted with a gas mixture used to simulate the scramjet engine exhaust flow at a free-stream Reynolds number of approximately 6.5 x 10(exp 6) per foot.
Cubbage, James M., Monta, William J.
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Feasibility study of hydrogen-ammonia synergistic combustion in scramjets across broad Mach ranges. [PDF]
Nat CommunSong X +6 more
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Pitot survey of exhaust flow field of a 2-D scramjet nozzle at Mach 6 with air or freon and argon used for exhaust simulation [PDF]
A pitot-rake survey of the simulated exhaust of a half-span scramjet nozzle model was conducted in the Langley 20-Inch Mach 6 Tunnel to provide an additional data set for computational fluid dynamics (CFD) code comparisons. A wind-tunnel model was tested
Monta, William J.
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A review of air-fuel mixing and alternative methods in scramjets and scramjet-like engines.
, 2016 This paper reviews work on two aspects of scramjet and similar ducted hypersonic propulsion. The first of these is air-fuel mixing techniques - the problem of mixing is considered the most intractable in scramjet design. The second aspect is the use of innovative techniques to supplement mixing or provide an alternative to combustion altogether.
Macleod, C., Gerrard, C.E.
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US hypersonics initiatives require accelerated efforts of the materials research community. [PDF]
MRS Bull, 2021 europepmc +1 more source