Melting heat transfer and entropy analysis of ternary Casson nanofluids flow with second slip conditions: Application on rocket engine cooling-Reference-Cited by-同舟云学术

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Melting heat transfer and entropy analysis of ternary Casson nanofluids flow with second slip conditions: Application on rocket engine cooling

Published:2024-09 Issue: Volume:102 Page:10-25
ISSN:1110-0168
Container-title:Alexandria Engineering Journal
language:en
Short-container-title:Alexandria Engineering Journal

Author:

Sayed Hamed M.^ORCID,Aly Emad H.^ORCID,Tharwat Marwa M.^ORCID,Mahros Amr M.^ORCID

Funder

King Abdulaziz University

Ministry of Education

Deanship of Scientific Research, Prince Sattam bin Abdulaziz University

Publisher

Elsevier BV

Reference70 articles.

1. Fundamental Concepts of Liquid-Propellant Rocket Engines;de Iaco Veris,2021

2. Modern engineering for design of liquid-propellant rocket engines;Huzel,1994

3. Rocket Propulsion;Heister,2019

4. Cooling process of liquid propellant rocket by means of kerosene-alumina nanofluid;Mahmoodi;Propul. Power Res.,2016

5. Rheological and thermophysical properties of ultra-stable kerosene based Fe3O4/Graphene nanofluids for energy conservation;Askari;Energy Convers. Manage.,2016

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