Experimental and comprehensive investigation of second throat diffuser area effect on ground test of a thrust optimized parabolic nozzle with different expansion ratios-Reference-Cited by-同舟云学术

Experimental and comprehensive investigation of second throat diffuser area effect on ground test of a thrust optimized parabolic nozzle with different expansion ratios

Published:2023-08 Issue: Volume:209 Page:146-158
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Fouladi Nematollah^ORCID,Afkhami Sina,Fard Mahmoud Pasandideh

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

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3. Transient three-dimensional side-loads analysis of a thrust-optimized parabolic nozzle during staging;Jia;Acta Astronaut.,2016

4. Numerical study of ways to prevent side loads in an over–expanded rocket nozzles during the launch stage;Ivanov;Acta Astronaut.,2019

5. The effect of second throat geometry on the performance of ejectors without induced flow;Bauer;AEDC-TDR-,1961

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3. Evaluation of generalized k-ω turbulence model in strong separated flow estimation of thrust optimized parabolic nozzle;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-08-21

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