Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line
type: Item
instance of: scholarly article
title: Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line
zbMATH Open document ID: 1242.76298
DOI: 10.1134/S001546281202010X
author: A. A. Krajko
author: A. N. Krajko
author: K. S. P'yankov
author: N. I. Tillyaeva
published in: Fluid Dynamics
publication date: 2012-07-02T00:00:00Z
Mathematics Subject Classification ID: 76N25
Mathematics Subject Classification ID: 76J20
zbMATH DE Number: 6051604
zbMATH Keywords: equalizing nozzle contour
zbMATH Keywords: intersections of \(C^{+}\) or \(C^{
zbMATH Keywords: }\)-characteristics
zbMATH Keywords: Mach number at the nozzle exit
zbMATH Keywords: the most rapid flow acceleration in the case of a curvilinear sonic line
MaRDI profile type: Publication
cites work: Effect of gas non-ideality on the performance of Laval nozzles with an abrupt constriction
cites work: Inviscid gas flows in nozzles with a steeply converging contour
cites work: Use of flows with straight sonic line in nozzles with corners
cites work: Supersonic ideal-gas flow of in the throat region of a nozzle
cites work: Q5850276
full work available at URL: s001546281202010x
OpenAlex ID: W2008805261
description: scientific article; zbMATH DE number 6051604