Conference on Physics of Entry Into Planetary Atmospheres 1963
DOI: 10.2514/6.1963-448
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Finite Difference Calculation of Hypersonic Wakes

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Cited by 14 publications
(8 citation statements)
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“…(1) in which j = 0, 1 for two-dimensional and axisymmetric flows, respectively, and x, u and y, v are streamwise and radial coordinates and associated velocities, respectively. Boundary and initial conditions on u are…”
Section: Discussionmentioning
confidence: 99%
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“…(1) in which j = 0, 1 for two-dimensional and axisymmetric flows, respectively, and x, u and y, v are streamwise and radial coordinates and associated velocities, respectively. Boundary and initial conditions on u are…”
Section: Discussionmentioning
confidence: 99%
“…P. RASTOGI,* KAUSHAL KISHORE,| AND N. L. MUNJALJ University of Gorakhpur, Gorakhpur, India M ANY nonhypergolic fuels can be made hypergolic by introducing suitable additives. 1 In some cases, introduction of a hot surface brings about ignition, which presumably makes use of the fact that the temperature is increased in the zone of reaction. Since ignition is preceded by oxidative degradation processes, it seems that these would be accelerated by the use of stronger oxidizing agents.…”
Section: Ignitability Of Nonhypergolic Propellants In Presence Of Potmentioning
confidence: 99%
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“…47). In these calculations, a value of K = 0.04 was used for all diffusivity models.^ Additionally, a laminar-turbulent transition calculation was performed.…”
Section: Turbulent Wake Calculationsmentioning
confidence: 93%
“…(4)(5)(6)(7)(8)(9)(10)(11) to the dynamical properties of the turbulence field, it is now necessary to establish a functional relationship between the local mean-square fluctuation intensity and the diffusive smearing rate. By invoking restriction 2, Sec.…”
Section: Governing Equation For \F/mentioning
confidence: 99%