Flow Characteristic Through Convergent-Divergent Nozzle
Keywords:
Mach Number, Sub-Sonic, Super-Sonic, Sonic, ThroatAbstract
In this paper, A nozzle is a device designed to control the direction or characteristics of a fluid flow (especially to increase velocity) as it exits (or enter) an enclosed chamber or pipe via orifice. A numerical study has been carried out to analyze the mass flow rate in terms of Pressure ratio, area ratio and mach number in the convergent-divergent nozzle.
References
- Robert W. Fox,Alan T.McDonald, Philip J.Prichart "Introduction to fluid Mechanics”.
- Dr.R.K.Bansal, "A TextBook of Fluid Mechanics and Hydraulic Machines”.
- Belgian patent no. 83,196 (issued: 1888 September 29)
- English patent no. 7143 (issued: 1889 April 29)
- de Laval, Carl Gustaf Patrik, "Steam turbine," U.S. Patent no. 522,066 (filed: 1889 May 1 ; issued: 1894 June 26)
- Flack, Ronald D. (June 2005). Fundamentals of Jet Propulsion with Applications. Cambridge University Press. Doi: 10.2277/0521819830. ISBN 978-0521819831.
- George P. Sutton (1992). Rocket Propulsion Elements: An Introduction to the Engineering of Rockets (6th ed.).
- Theodore Stevens and Henry M. Hobart (1906). Steam Turbine Engineering. MacMillan Company. pp. 24–27.
- Andrew Johnson and Dimitri Papamoschou,” Shock Motion And Flow Instabilities In Supersonic Nozzle Flow Separation”, University of California, Irvine, Irvine, CA, 92697-3975
- Lewis, C. H., Jr., and Carlson, D. J., "Normal Shock Location Inunder expanded Gas And Gas Particle Jets,” AIAA Journal, Vol 2, No.4,April 1964, pp. 776-777.
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