Numerical simulation of shock-induced separated flows in overexpanded rocket nozzles
Published online: 2013-01-29
Articles citing this article
The Citing articles tool gives a list of articles citing the current article.
The citing articles come from EDP Sciences database, as well as other publishers participating in CrossRef Cited-by Linking Program. You can set up your personal account to receive an email alert each time this article is cited by a new article (see the menu on the right-hand side of the abstract page).
Cited article:
This article has been cited by the following article(s):
Computational investigation of cooling effectiveness for film cooled dual-bell exhaust nozzle for LO2/LH2 liquid rocket engines
Martin Raju, Abhilash Suryan and David ŠimurdaEnergy Sources, Part A: Recovery, Utilization, and Environmental Effects 47 (1) 10315 (2025)
https://doi.org/10.1080/15567036.2021.1963885
Gas dynamics at starting and terminating phase of a supersonic exhaust diffuser with a conical nozzle
Sina Afkhami and Nematollah FouladiPhysics of Fluids 36 (3) (2024)
https://doi.org/10.1063/5.0197296
Experimental and comprehensive investigation of second throat diffuser area effect on ground test of a thrust optimized parabolic nozzle with different expansion ratios
Nematollah Fouladi, Sina Afkhami and Mahmoud Pasandideh FardActa Astronautica 209 146 (2023)
https://doi.org/10.1016/j.actaastro.2023.05.004
Starting transient analysis of second throat exhaust diffuser in high-altitude test of a thrust optimized parabolic nozzle
Nematollah Fouladi, Sina Afkhami and Mahmoud Pasandideh FardPhysics of Fluids 35 (6) (2023)
https://doi.org/10.1063/5.0154030
Comparative analysis of 2D simulations and isentropic equations for compressible flow in experimental nozzles
San Luis TOLENTINOINCAS BULLETIN 15 (3) 111 (2023)
https://doi.org/10.13111/2066-8201.2023.15.3.9
Experimental and numerical investigation of transient starting of pre-evacuated exhaust diffuser in high altitude ground test
Sina Afkhami, Nematollah Fouladi and Mahmoud Pasandideh FardAerospace Science and Technology 133 108111 (2023)
https://doi.org/10.1016/j.ast.2023.108111
Evaluation of generalized k-ω turbulence model in strong separated flow estimation of thrust optimized parabolic nozzle
Sina Afkhami, Nematollah Fouladi and Mahmoud PasandidehFardProceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 237 (14) 3143 (2023)
https://doi.org/10.1177/09544100231195774
Numerical investigation of second throat exhaust diffuser performance with thrust optimized parabolic nozzles
N. Fouladi and M. FarahaniAerospace Science and Technology 105 106020 (2020)
https://doi.org/10.1016/j.ast.2020.106020
31st International Symposium on Shock Waves 2
A. Sansica, J.-Ch. Robinet, Eric Goncalves and J. Herpe31st International Symposium on Shock Waves 2 523 (2019)
https://doi.org/10.1007/978-3-319-91017-8_67
Parametric study of supersonic film cooling in dual bell nozzle for an experimental air–kerosene engine
Siba Prasad Choudhury, Abhilash Suryan, J.C. Pisharady, A. Jayashree and Khalid RashidAerospace Science and Technology 78 364 (2018)
https://doi.org/10.1016/j.ast.2018.04.038