Numerical simulation of rocket nozzle

G. Srinivas, Srinivasa Rao Potti

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The vent or opening is called nozzle. The objectives are to measure the flow rates and pressure distributions within the converging and diverging nozzle under different exit and inlet pressure ratios. Analytic results will be used to contrast the measurements for the pressure and normal shock locations. In this paper computational Fluid Dynamics (CFD) Analysis of various performance parameters like static pressure, the Mach number, intensity of turbulence, the area ratio are studied in detail for a rocket nozzle from Inlet to exit by using Ansys Fluent software. From the public literature survey the geometry co-ordinates are taken. The throat diameter and exit and diameter are same for all nozzles. After the simulation the results revealed that the divergence angle varies the mach number and other performance parameters also varies. For smaller nozzle angle the discharge coefficient increases with increasing pressure ratio until the choked condition is reached for varying the divergence angle.

Original languageEnglish
Title of host publicationModern Achievements and Developments in Manufacturing and Industry
PublisherTrans Tech Publications Ltd
Pages1210-1213
Number of pages4
ISBN (Print)9783038351481
DOIs
Publication statusPublished - 01-01-2014
Externally publishedYes
Event2014 International Conference on Recent Advances in Mechanical Engineering and Interdisciplinary Developments, ICRAMID 2014 - Tamil Nadu, India
Duration: 07-03-201408-03-2014

Publication series

NameAdvanced Materials Research
Volume984-985
ISSN (Print)1022-6680
ISSN (Electronic)1662-8985

Conference

Conference2014 International Conference on Recent Advances in Mechanical Engineering and Interdisciplinary Developments, ICRAMID 2014
CountryIndia
CityTamil Nadu
Period07-03-1408-03-14

Fingerprint

Rocket nozzles
Nozzles
Computer simulation
Mach number
Vents
Pressure distribution
Dynamic analysis
Computational fluid dynamics
Turbulence
Flow rate
Geometry

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Srinivas, G., & Potti, S. R. (2014). Numerical simulation of rocket nozzle. In Modern Achievements and Developments in Manufacturing and Industry (pp. 1210-1213). (Advanced Materials Research; Vol. 984-985). Trans Tech Publications Ltd. https://doi.org/10.4028/www.scientific.net/AMR.984-985.1210
Srinivas, G. ; Potti, Srinivasa Rao. / Numerical simulation of rocket nozzle. Modern Achievements and Developments in Manufacturing and Industry. Trans Tech Publications Ltd, 2014. pp. 1210-1213 (Advanced Materials Research).
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Srinivas, G & Potti, SR 2014, Numerical simulation of rocket nozzle. in Modern Achievements and Developments in Manufacturing and Industry. Advanced Materials Research, vol. 984-985, Trans Tech Publications Ltd, pp. 1210-1213, 2014 International Conference on Recent Advances in Mechanical Engineering and Interdisciplinary Developments, ICRAMID 2014, Tamil Nadu, India, 07-03-14. https://doi.org/10.4028/www.scientific.net/AMR.984-985.1210

Numerical simulation of rocket nozzle. / Srinivas, G.; Potti, Srinivasa Rao.

Modern Achievements and Developments in Manufacturing and Industry. Trans Tech Publications Ltd, 2014. p. 1210-1213 (Advanced Materials Research; Vol. 984-985).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Srinivas G, Potti SR. Numerical simulation of rocket nozzle. In Modern Achievements and Developments in Manufacturing and Industry. Trans Tech Publications Ltd. 2014. p. 1210-1213. (Advanced Materials Research). https://doi.org/10.4028/www.scientific.net/AMR.984-985.1210