Finite Difference Calculation of Hypersonic Wakes

Approximate analysis of free-mixing flows

“…(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…”

“…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.…”

“…1 ' 2 Although such methods are necessary to predict flow properties in chemically reacting nonequilibrium flows, their use for less complex flow problems may be prohibited by high computer expense; it is then desirable to have available means to develop accurate approximate solutions.…”

Finite-difference calculation of hypersonic wakes

“…47). In these calculations, a value of K = 0.04 was used for all diffusivity models.^ Additionally, a laminar-turbulent transition calculation was performed.…”

A bimodal approximation for reacting turbulent flows. I - Description of the model.

“…(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.…”