Design anatomization & numerical simulation of nozzle with exit deflection angle in scramjet-Reference-Cited by-同舟云学术

Design anatomization & numerical simulation of nozzle with exit deflection angle in scramjet

Published:2023 Issue: Volume: Page:
ISSN:0094-243X
Container-title:MACHINE LEARNING AND INFORMATION PROCESSING: PROCEEDINGS OF ICMLIP 2023
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Author:

Patel Mansha Kumari B.,Lad Bhavini H.,Makadia Dharmik L.,Panchal Ayushbhai K.,Patel Akshit G.

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0168866

Reference10 articles.

1. Andrew Ridgway, Ashish Alex Sam & Apostolos Pesyridis. 2018. “Modelling a Hypersonic Single Expansion Ramp Nozzle of a Hypersonic Aircraft through Parametric Studies”, Brunel University London, London (UK) 11–3449.

2. S. Vivek, M. Sathiyaseelan, G. Suresh, G. Muthu & S. Srinivasan. 2019. “Performance Analysis of Scramjet Engine with Different Nozzle Angles”, Journal of Advanced Engineering Research (JAER), Chennai (India) Vol. 6 (Issue.2).

3. Ramesha D.K., Rudra Murthy & Hemanth Kumar. P,. 2013, “CFD Analysis of Supersonic Exhaust in a Scramjet Engine’, International Journal of Innovative Research in Science, Engineering and Technology (IJIRSET), Bangalore (India) Vol. 2 (Issue.9).

4. Dr. S. Nagakalyan, M. Satya Prasad & Mohammad Arif Hussain,. 2019. “Design and Flow Analysis of Various Convergent – Divergent Nozzle by using Computational Fluid Dynamics”, International Journal of Industrial Research and Applied Engineering (JIRAE), Chennai (India) Vol. 6 (Issue.5)

5. Richard L. Gaffney, Jr John J. Kortet, 2004, “Analysis and Design of Rectangular Cross Section Nozzle for Scramjet Engine Testing”, American Institute Aeronautics and Astronautics, NASA-Langley, AIAA. 2004–1137.