HYPERSONIC NUZZLE DESIGN FOR VISCOUS REAL GAS FLOW

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SOLTANI M.R.; FARHAT M.

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Paper Information

Journal: JOURNAL OF AEROSPACE SCIENCE AND RESEARCH Year:2009 | Volume:2 | Issue:2 Page(s): 39-47

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Information Journal Paper

Title

HYPERSONIC NUZZLE DESIGN FOR VISCOUS REAL GAS FLOW

Author(s)

SOLTANI M.R. | FARHAT M. | Issue Writer Certificate

Keywords

MACH NUMBERQ3

HYPERSONIC FLOW REGIMEQ3

CONVERGENT-DIVERGENT NOZZLEQ3

FOELSCH’S METHODQ3

BOUNDARY LAYER DISPLACEMENT THICKNESSQ3

Abstract

In this paper, the divergent part of a two dimension nozzle of an intermittent blow-down hypersonic wind tunnel capable for maximum MACH NUMBER of 7 is designed. The real gas and viscous effects are taken into account in determination of nozzle contour. Finally, by using Foelsch method as an analytical method for designing hypersonic nozzle contour, a CFD code has been presented and the results of this code are attached.

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APA: Copy

SOLTANI, M.R., & FARHAT, M.. (2009). HYPERSONIC NUZZLE DESIGN FOR VISCOUS REAL GAS FLOW. JOURNAL OF AEROSPACE SCIENCE AND RESEARCH, 2(2), 39-47. SID. https://sid.ir/paper/199473/en

Vancouver: Copy

SOLTANI M.R., FARHAT M.. HYPERSONIC NUZZLE DESIGN FOR VISCOUS REAL GAS FLOW. JOURNAL OF AEROSPACE SCIENCE AND RESEARCH[Internet]. 2009;2(2):39-47. Available from: https://sid.ir/paper/199473/en

IEEE: Copy

M.R. SOLTANI, and M. FARHAT, “HYPERSONIC NUZZLE DESIGN FOR VISCOUS REAL GAS FLOW,” JOURNAL OF AEROSPACE SCIENCE AND RESEARCH, vol. 2, no. 2, pp. 39–47, 2009, [Online]. Available: https://sid.ir/paper/199473/en

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