Computational Analysis of a Convergent Divergent Nozzle

Author:

Pothala Srinivas,Raju M. V. Jagannadha,Bangarraju B.,Lakshmi Narayana V.

Publisher

Springer Nature Singapore

Reference13 articles.

1. Boyanapalli R, Vanukuri RSR, Gogineni P, Nookala J, Yarlagadda GK, Gada V (2013) Analysis of composite De-Laval nozzle suitable for rocket applications. Int J Innovative Technol Exploring Eng 2:336–344

2. Hoffman JD, Thompson HD, Marcum DL, Purdue Univ., West Lafayette. In: An analytical investigation of the effects of Swirler design on the performance of annular propulsive nozzles, AIAA-1984-0282

3. Rychkov D, Calculation of the swirling flow of an ideal gas in a de laval nozzle, UDC 533.6.011

4. Allé NK (2016) 2800 Kgs, CFD modelling of particle behaviour in supersonic flows with strong swirls for gas separation. In: Separation and purification technology, Science direct, Denmark vol 168, pp 68–73

5. Luca F (2006) A study on axially rotating pipe and swirling jet flows. Technical Reports from Royal Institute of Technology, Sweden

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