Parametric study on a method to control flow separation in rocket nozzles-Reference-Cited by-同舟云学术

Parametric study on a method to control flow separation in rocket nozzles

Published:2021 Issue: Volume:46 Page:9950-9955
ISSN:2214-7853
Container-title:Materials Today: Proceedings
language:en
Short-container-title:Materials Today: Proceedings

Author:

Sreerag VN,Mohammad Fazil,Nandan Vishnu,Pramod Anurag,Subhajayan KP.,Jash Samik

Publisher

Elsevier BV

Subject

General Medicine

Reference22 articles.

1. Numerical prediction of nozzle flow separation: issues of turbulence modeling;Allamaprabhu;Aerosp. Sci. Technol.,2016

2. Jans Ostlund, Flow Processes in Rocket Engine Nozzles with Focus on Flow Separation and Side-Loads, Technical Report 2002:09, May 2002.

3. Solving the flow separation issue: a new nozzle concept;Boccaletto,2008

4. Pallav Kant Joseph Mathew Estimation of transition in dual bell nozzle operation, Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, Bangalore, India.

5. Fluent Inc., FLUENT 6.3 User’s Guide

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