Parametric study of supersonic film cooling in dual bell nozzle for an experimental air–kerosene engine-Reference-Cited by-同舟云学术

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Parametric study of supersonic film cooling in dual bell nozzle for an experimental air–kerosene engine

Published:2018-07 Issue: Volume:78 Page:364-376
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Choudhury Siba Prasad,Suryan Abhilash,Pisharady J.C.,Jayashree A.,Rashid Khalid

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference54 articles.

1. Advanced rocket nozzles;Hagemann;J. Propuls. Power,1998

2. Experimental Study of Gas-Flow Separation in Overexpanded Exhaust Nozzles for Rocket Motors;Foster,1949

3. Dual-Bell Altitude Compensating Nozzles;Horn,1994

4. Experimental Comparison of Dual Bell and Expansion Deflection Nozzles;Taylor,2011

5. Reynolds number influence on dual-bell transition phenomena;Verma;J. Propuls. Power,2013

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