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Validation of Supersonic Film Cooling Modeling for Liquid Rocket Engine Applications (in English)
Nasa Technical Reports Server (Ntrs)
(Author)
·
Christopher I. Morris
(Author)
·
Joseph H. Ruf
(Author)
·
Bibliogov
· Paperback
Validation of Supersonic Film Cooling Modeling for Liquid Rocket Engine Applications (in English) - Morris, Christopher I. ; Ruf, Joseph H. ; Nasa Technical Reports Server (Ntrs)
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Synopsis "Validation of Supersonic Film Cooling Modeling for Liquid Rocket Engine Applications (in English)"
Topics include: upper stage engine key requirements and design drivers; Calspan "stage 1" results, He slot injection into hypersonic flow (air); test articles for shock generator diagram, slot injector details, and instrumentation positions; test conditions; modeling approach; 2-d grid used for film cooling simulations of test article; heat flux profiles from 2-d flat plate simulations (run #4); heat flux profiles from 2-d backward facing step simulations (run #43); isometric sketch of single coolant nozzle, and x-z grid of half-nozzle domain; comparison of 2-d and 3-d simulations of coolant nozzles (run #45); flowfield properties along coolant nozzle centerline (run #45); comparison of 3-d CFD nozzle flow calculations with experimental data; nozzle exit plane reduced to linear profile for use in 2-d film-cooling simulations (run #45); synthetic Schlieren image of coolant injection region (run #45); axial velocity profiles from 2-d film-cooling simulation (run #45); coolant mass fraction profiles from 2-d film-cooling simulation (run #45); heat flux profiles from 2-d film cooling simulations (run #45); heat flux profiles from 2-d film cooling simulations (runs #47, #45, and #47); 3-d grid used for film cooling simulations of test article; heat flux contours from 3-d film-cooling simulation (run #45); and heat flux profiles from 3-d and 2-d film cooling simulations (runs #44, #46, and #47).
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The book is written in English.
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