Titlebook: Numerical Simulation of Viscous Shock Layer Flows; Yuri P. Golovachov Book 1995 Springer Science+Business Media B.V. 1995 Navier-Stokes eq

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书目名称Numerical Simulation of Viscous Shock Layer Flows影响因子(影响力)




书目名称Numerical Simulation of Viscous Shock Layer Flows影响因子(影响力)学科排名




书目名称Numerical Simulation of Viscous Shock Layer Flows网络公开度




书目名称Numerical Simulation of Viscous Shock Layer Flows网络公开度学科排名




书目名称Numerical Simulation of Viscous Shock Layer Flows被引频次




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LUCY

https://doi.org/10.1007/978-94-015-8490-6Navier-Stokes equation; dynamics; heat transfer; numerical methods; simulation

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978-90-481-4594-2Springer Science+Business Media B.V. 1995

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Numerical Simulation of Viscous Shock Layer Flows978-94-015-8490-6Series ISSN 0926-5112 Series E-ISSN 2215-0056

Collision

Viscous shock layer models and computational methods,Such calculations can be carried out not only with the full Navier-Stokes equations but also with more simple mathematical models whose implementation requires a substantially smaller amount of computations.

Commodious

Applications to plane and axisymmetric flows,er models. Most of them pertained to stationary flows about the bodies of revolution placed in a uniform supersonic stream. This chapter deals with simulation of more complicated viscous shock layer flows.

forager

Simulation of three-dimensional flows,evere restrictions on the allowable value of time increment and the lower convergence rate of the iterative procedures as compared with one- and two-dimensional problems. For this reason, the well-founded use of gas dynamic models and numerical methods appears to be especially important.

休息

Physical and chemical effects,ve physical and chemical processes which considerably influence the shock layer flow field and heat transfer. The examples of calculations are presented pertaining to spacecraft flight in the Earth and other planet atmospheres.

阶层

Book 1995irst of all, by aviation and aerospace engineering. The designing of aircraft and space vehicles requires a more precise prediction of the aerodynamic and heat transfer characteristics. Together with broadening of the flight condition range, this makes it necessary to take into account a number of g

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