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The Interaction of a Hypersonic Plume with an External Hypersonic Stream
1973Abstract : A theoretical study of the gas dynamic interaction between a hypersonic plume and the opposed hypersonic external stream is presented. Steady, axisymmetric, inviscid, perfect gas flow is postulated for both the bow and far field regions.
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Il Nuovo Cimento, 1955
Methods of mixed fields are extended to the case of hyperons. In order to take into account a new particle (Y-particle) which decays into a Λ-particle and a π-meson, a set of the so-called strong interactions between hyperson and mesons is assumed. Then the Λ-particle self-energy is calculated to the second-order terms through the use of the method of ...
H. Enatsu, C. Ihara
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Methods of mixed fields are extended to the case of hyperons. In order to take into account a new particle (Y-particle) which decays into a Λ-particle and a π-meson, a set of the so-called strong interactions between hyperson and mesons is assumed. Then the Λ-particle self-energy is calculated to the second-order terms through the use of the method of ...
H. Enatsu, C. Ihara
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1962
An experimental investigation was made of the flow field behind a two-dimensional circular cylinder at a nominal Mach number of 5.7. The free-stream Reynolds number based on the cylinder diameter was varied over a range from 4300 to 66, 500 by changing both the diameter of the cylinder and the stagnation pressure of the wind tunnel.
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An experimental investigation was made of the flow field behind a two-dimensional circular cylinder at a nominal Mach number of 5.7. The free-stream Reynolds number based on the cylinder diameter was varied over a range from 4300 to 66, 500 by changing both the diameter of the cylinder and the stagnation pressure of the wind tunnel.
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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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Will there or will there not be a hypersonic airplane?
Journal of Engineering Physics and Thermophysics, 2000An analytical overview of the problems of heat transfer occurring in horizontal flight of a body in the earth’s atmosphere at a hypersonic speed is given. It is shown that, despite the enormous experience accumulated in the design and development of shuttle systems (Space Shuttle, Buran), the creation of a hypersonic airplane still remains a serious ...
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INTERACTIONS BETWEEN A HYPERSONIC WAKE AND A FOLLOWING HYPERSONIC PROJECTILE
AIAA Journal, 1963R. E. SLATTERY +2 more
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Sublimation in a Hypersonic Environment
Journal of the Aerospace Sciences, 1960openaire +2 more sources