Development of Gas Dynamic Nozzles: A Preliminary Computational Study-Reference-Cited by-同舟云学术

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Development of Gas Dynamic Nozzles: A Preliminary Computational Study

Published:2024-01-09 Issue: Volume:74 Page:151
ISSN:
Container-title:RAiSE-2023
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Author:

Savanur Prasad¹^ORCID,Venu Ganapuram²,Kumar G. N.¹,Ramaprasad M. V.³,Uttarwar Padmavati K.³

Affiliation:

1. Department of Mechanical Engineering, National Institute of Technology Karnataka, Surathkal 575025, Karnataka, India

2. CSIR-National Aerospace Laboratories, Bengaluru 560017, Karnataka, India

3. GITAM School of Business Bengaluru, GITAM University, Bengaluru 561203, Karnataka, India

Publisher

MDPI

Link

https://www.mdpi.com/2673-4591/59/1/151/pdf

Reference20 articles.

1. Deere, K.A., Berrier, B.L., Flamm, J.D., and Johnson, S.K. (2005, January 10–13). A Computational Study of a New Dual Throat Fluidic Thrust Vectoring Nozzle Concept. Proceedings of the 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona. AIAA Paper 2005-3502.

2. Numerical Exploration of Transverse Sonic Jet In Hypersonic Cross-flow;Bhati;J. Aerosp. Sci. Technol.,2022

3. Time evolution and mixing characteristics of hydrogen and ethylene transverse jets in supersonic crossflows;Mungal;Phys. Fluids,2006

4. Resta, E., Marsilio, R., and Ferlauto, M. (2021). Thrust Vectoring of a Fixed Axisymmetric Supersonic Nozzle Using the Shock-Vector Control Method. Fluids, 6.

5. Sharma, V., Chakraborty, D., and Eswaran, V. (2018, January 10–12). Computational Study of Sonic Injection in Supersonic Crossflow. Proceedings of the 7th International and 45th National Conference on Fluid Mechanics and Fluid Power (FMFP), IIT Bombay, Mumbai, India.

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