Experimental and numerical investigation of transient starting of pre-evacuated exhaust diffuser in high altitude ground test-Reference-Cited by-同舟云学术

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Experimental and numerical investigation of transient starting of pre-evacuated exhaust diffuser in high altitude ground test

Published:2023-02 Issue: Volume:133 Page:108111
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Afkhami Sina,Fouladi Nematollah,Pasandideh Fard Mahmoud^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

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2. Approximation of optimum thrust nozzle contour;Rao;ARS J.,1960

3. Sea level side loads in high-area-ratio rocket engines;Nave,1973

4. Numerical simulation of shock-induced separated flows in over-expanded rocket nozzles;Shams;Prog. Flight Phys.,2012

5. A study of the supersonic ejector–diffuser system with an inlet orifice;Lijo;Aerosp. Sci. Technol.,2012

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1. Experimental evaluation of the influence of the diffuser inlet to nozzle exit cross sectional area ratio on pressure oscillation in a high-altitude test facility;Physics of Fluids;2024-08-01

2. Gas dynamics at starting and terminating phase of a supersonic exhaust diffuser with a conical nozzle;Physics of Fluids;2024-03-01

3. Research on fault diagnosis technology of simulated altitude test facility based on multi-optimization strategy, real-time data transfer, and the M-H attention-RF algorithm;Multimedia Tools and Applications;2023-09-07

4. 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

5. Experimental and comprehensive investigation of second throat diffuser area effect on ground test of a thrust optimized parabolic nozzle with different expansion ratios;Acta Astronautica;2023-08

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