Flow regimes formed by a counterflow jet in a supersonic flow
type: Item
instance of: scholarly article
zbMATH Open document ID: 0983.76045
author: V. M. Fomin
author: A. P. Shashkin
author: T. A. Korotaeva
author: N. D. Malmuth
author: A. A. Maslov
publication date: 2001-12-13T00:00:00Z
Mathematics Subject Classification ID: 76J20
Mathematics Subject Classification ID: 76M12
zbMATH DE Number: 1682328
zbMATH Keywords: counterflow jet
zbMATH Keywords: inviscid gas
zbMATH Keywords: finite volume method
zbMATH Keywords: dynamic pressure
zbMATH Keywords: maximal drag reduction
zbMATH Keywords: Mach number
zbMATH Keywords: supersonic flow
MaRDI profile type: Publication
title: Flow regimes formed by a counterflow jet in a supersonic flow
published in: Prikladnaya Mekhanika i Tekhnicheskaya Fizika
review text: The authors investigate the effects of dynamic pressure, Mach number and temperature of a jet injected from a body upstream of a free supersonic flow on the formation of the flow around the body. In particular, the authors identify the flow regimes which provide the maximal drag reduction, and give an approximate criterion which allows to estimate the applicability of various models of jet penetration into the flow.
description: scientific article; zbMATH DE number 1682328