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Effect of Kerosene Dual-Jet Spacing on the Mixing and Combustion Characteristics of a Scramjet Combustor. [PDF]
ACS OmegaPeng SS +5 more
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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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Journal of Applied Mechanics, 1974
Apart from method of characteristic calculations, there has been little analytical consideration of high-speed internal flows where transverse curvature and/or viscous-inviscid interaction are important. Molder [1] has carried out a numerical computation for internal conical flow using the inviscid Taylor-Macoll equations; however, a singular ray is ...
Lin, T. C., Rubin, S. G.
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Apart from method of characteristic calculations, there has been little analytical consideration of high-speed internal flows where transverse curvature and/or viscous-inviscid interaction are important. Molder [1] has carried out a numerical computation for internal conical flow using the inviscid Taylor-Macoll equations; however, a singular ray is ...
Lin, T. C., Rubin, S. G.
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Panel flutter in hypersonic flow.
AIAA Journal, 1967IV," Transactions of the American Society for Metals, Transactions Quarterly, Vol. 59, 1966, p. 876. Fager D. N. and Spur W. F., "Some Characteristics of Aqueous Stress Corrosion in Titanium Alloys," Document D660083, Sept. 1967, The Boeing Co. 11 Beck, T. R., "Stress Corrosion Cracking of Titanium Alloys, II.
Bailie, J. A., McFeely, J. E.
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Design Optimization in Hypersonic Flows
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, 2012The objective of this study is to develop a reliabl e and efficient design tool that can be used in hyp ersonic flows. The flow analysis is based on axisymmetric Euler an d the finite rate chemical reaction equations. Thes e coupled equations are solved by using Newton’s method.
Eyi, Sinan, Yumuşak, M.
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AIAA Journal, 1970
Abstract : A study of the motions of solid particles in a dusty gas in the inviscid hypersonic shock layers of slender wedges and cones and the stagnation regions of cylinders and spheres is carried out. Particles of uniform size and with a size distribution are considered.
RONALD F. PROBSTEIN, FRANCO FASSIO
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Abstract : A study of the motions of solid particles in a dusty gas in the inviscid hypersonic shock layers of slender wedges and cones and the stagnation regions of cylinders and spheres is carried out. Particles of uniform size and with a size distribution are considered.
RONALD F. PROBSTEIN, FRANCO FASSIO
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2015
Abstract The chapter starts its analysis with blunt-nosed bodies. In a supersonic flow, a blunt-nosed body produces a bow shock wave. The chapter shows that the shape of the shock and the entire flow between the shock and the body become independent of the Mach number, M∞, provided it is large enough.
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Abstract The chapter starts its analysis with blunt-nosed bodies. In a supersonic flow, a blunt-nosed body produces a bow shock wave. The chapter shows that the shape of the shock and the entire flow between the shock and the body become independent of the Mach number, M∞, provided it is large enough.
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Similarity Laws of Hypersonic Flows
Journal of Mathematics and Physics, 1946Not ...
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