Flow Characteristic Through Convergent-Divergent Nozzle

Authors(3) :-S. Sathyapriya, R. Swathi, P. Bavya Seeli

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.

Authors and Affiliations

S. Sathyapriya
Assistant Professor of Sri Krishna Arts And Science College. Coimbatore, TamilNadu, India
R. Swathi
Sri Krishna Arts and Science College, Coimbatore, TamilNadu, India
P. Bavya Seeli
Sri Krishna Arts and Science College, Coimbatore, TamilNadu, India

Mach Number, Sub-Sonic, Super-Sonic, Sonic, Throat

  1. Robert W. Fox,Alan T.McDonald, Philip J.Prichart "Introduction to fluid Mechanics”.
  2. Dr.R.K.Bansal, "A TextBook of Fluid Mechanics and Hydraulic Machines”.
  3. Belgian patent no. 83,196 (issued: 1888 September 29)
  4. English patent no. 7143 (issued: 1889 April 29)
  5. de Laval, Carl Gustaf Patrik, "Steam turbine," U.S. Patent no. 522,066 (filed: 1889 May 1 ; issued: 1894 June 26)
  6. Flack, Ronald D. (June 2005). Fundamentals of Jet Propulsion with Applications. Cambridge University Press. Doi: 10.2277/0521819830. ISBN 978-0521819831.
  7. George P. Sutton (1992). Rocket Propulsion Elements: An Introduction to the Engineering of Rockets (6th ed.).
  8. Theodore Stevens and Henry M. Hobart (1906). Steam Turbine Engineering. MacMillan Company. pp. 24–27.
  9. Andrew Johnson and Dimitri Papamoschou,” Shock Motion And Flow Instabilities In Supersonic Nozzle Flow Separation”, University of California, Irvine, Irvine, CA, 92697-3975
  10. 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.

Publication Details

Published in : Volume 4 | Issue 2 | January-February 2018
Date of Publication : 2018-02-28
License:  This work is licensed under a Creative Commons Attribution 4.0 International License.
Page(s) : 896-901
Manuscript Number : IJSRST1841207
Publisher : Technoscience Academy

Print ISSN : 2395-6011, Online ISSN : 2395-602X

Cite This Article :

S. Sathyapriya, R. Swathi, P. Bavya Seeli, " Flow Characteristic Through Convergent-Divergent Nozzle", International Journal of Scientific Research in Science and Technology(IJSRST), Print ISSN : 2395-6011, Online ISSN : 2395-602X, Volume 4, Issue 2, pp.896-901, January-February-2018.
Journal URL : https://ijsrst.com/IJSRST1841207
Citation Detection and Elimination     |      | |
  • 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.
  • " target="_blank"> BibTeX
    |
  • 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.
  • " target="_blank">RIS
    |
  • 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.
  • " target="_blank">CSV

    Article Preview