Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6. 80
type: Item
instance of: scholarly article
title: Numerical analysis of pressure oscillations over axisymmetric spiked blunt bodies at Mach 6. 80
zbMATH Open document ID: 1031.76031
author: R. C. Mehta
published in: Shock Waves
publication date: 2002-09-10T00:00:00Z
review text: The pressure oscillations occuring in the hypersonic flow around an axisymmetric blunt body equipped with a spike are computed by a numerical finite volume method. The numerical results are compared to experimental data, and a spectral analysis is performed.
reviewed by: Thomas Sonar
Mathematics Subject Classification ID: 76M12
Mathematics Subject Classification ID: 76K05
zbMATH DE Number: 1798910
zbMATH Keywords: hypersonic flow
zbMATH Keywords: separated flows
zbMATH Keywords: spectral analysis
zbMATH Keywords: axisymmetric blunt body
zbMATH Keywords: spike
zbMATH Keywords: finite volume method
MaRDI profile type: Publication
full work available at URL: s001930200127
OpenAlex ID: W1986930822
DOI: 10.1007/S001930200127
description: scientific article; zbMATH DE number 1798910