Axisymmetric shock wave interaction with a cone: a benchmark test


Autoria(s): Sun, M; Saito, T; Jacobs, PA; Timofeev, EV; Ohtani, K; Takayama, K
Contribuinte(s)

K Takayama (Editor-in-Chief)

Y Horie (Managing Editor)

Data(s)

01/01/2005

Resumo

Results of the benchmark test are presented of comparing numerical schemes solving shock wave of M-s = 2.38 in nitrogen and argon interacting with a 43 degrees semi-apex angle cone and corresponding experiments. The benchmark test was announced in Shock Waves Vol. 12, No. 4, in which we tried to clarify the effects of viscosity and heat conductivity on shock reflection in conical flows. This paper summarizes results of ten numerical and two experimental applications. State of the art in studies regarding the shock/cone interaction is clarified.

Identificador

http://espace.library.uq.edu.au/view/UQ:77744

Idioma(s)

eng

Publicador

Springer-Verlag

Palavras-Chave #Shock Wave Reflection #Axial Symmetry #Cone #Nechmark Tst #Viscosity #Heat Conductivity #Mechanics #Benchmark Test #Multidimensional Compressible Flows #Monotonic Numerical-methods #Reflection #Efficient #Equations #Accurate #Scheme #Cfd #C1 #780102 Physical sciences #290299 Aerospace Engineering not elsewhere classified
Tipo

Journal Article