Steady, shock-capturing method applied to one-dimensional nozzle flow

S. Parameswaran

doi:10.2514/3.10259

Steady, shock-capturing method applied to one-dimensional nozzle flow

S. Parameswaran

Mechanical Engineering

Research output: Contribution to journal › Article › peer-review

1 Scopus citations

Original language	English
Pages (from-to)	1292-1295
Number of pages	4
Journal	AIAA Journal
Volume	27
Issue number	9
DOIs	https://doi.org/10.2514/3.10259
State	Published - Sep 1989

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@article{a6b85657895f4347b5e28a5920fcc160,

title = "Steady, shock-capturing method applied to one-dimensional nozzle flow",

author = "S. Parameswaran",

note = "Funding Information: Support of P. S. Bernard for this study was provided in part through an American Society for Engineering Education/ Navy Summer Faculty Research Fellowship. Funding Information: This work was performed at the Computational Fluid Dynamics Unit of the Imperial College, London, and was supported by a Commonwealth Scholarship. The author wishes to thank Professor Brian Spalding and Dr. George Carroll for their helpful discussions and enthusiasm.",

year = "1989",

month = sep,

doi = "10.2514/3.10259",

language = "English",

volume = "27",

pages = "1292--1295",

journal = "AIAA Journal",

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number = "9",

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T1 - Steady, shock-capturing method applied to one-dimensional nozzle flow

AU - Parameswaran, S.

N1 - Funding Information: Support of P. S. Bernard for this study was provided in part through an American Society for Engineering Education/ Navy Summer Faculty Research Fellowship. Funding Information: This work was performed at the Computational Fluid Dynamics Unit of the Imperial College, London, and was supported by a Commonwealth Scholarship. The author wishes to thank Professor Brian Spalding and Dr. George Carroll for their helpful discussions and enthusiasm.

PY - 1989/9

Y1 - 1989/9

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U2 - 10.2514/3.10259

DO - 10.2514/3.10259

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SP - 1292

EP - 1295

JO - AIAA Journal

JF - AIAA Journal

SN - 0001-1452

IS - 9

ER -

Steady, shock-capturing method applied to one-dimensional nozzle flow

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