Approximate solutions for the structure of shock waves


Autoria(s): Ananthasayanam, MR; Narasimha, R
Data(s)

01/03/1969

Resumo

Approximate solutions of the B-G-K model equation are obtained for the structure of a plane shock, using various moment methods and a least squares technique. Comparison with available exact solution shows that while none of the methods is uniformly satisfactory, some of them can provide accurate values for the density slope shock thickness delta n . A detailed error analysis provides explanations for this result. An asymptotic analysis of delta n for largeMach numbers shows that it scales with theMaxwell mean free path on the hot side of the shock, and that their ratio is relatively insensitive to the viscosity law for the gas.

Formato

application/pdf

Identificador

http://eprints.iisc.ernet.in/27649/1/33.pdf

Ananthasayanam, MR and Narasimha, R (1969) Approximate solutions for the structure of shock waves. In: Acta Mechanica, 7 (1). pp. 1-15.

Publicador

Springer

Relação

http://www.springerlink.com/content/v751087023t50854/

http://eprints.iisc.ernet.in/27649/

Palavras-Chave #Aerospace Engineering (Formerly, Aeronautical Engineering)
Tipo

Journal Article

PeerReviewed