NDLI: Injector design tool improvements: user's manual for fdns v.4.5

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Injector design tool improvements: user's manual for fdns v.4.5

Content Provider	NASA Technical Reports Server (NTRS)
Author	Chen, Yen-Sen Shang, Huan-Min Wei, Hong Liu, Jiwen
Copyright Year	1998
Description	The major emphasis of the current effort is in the development and validation of an efficient parallel machine computational model, based on the FDNS code, to analyze the fluid dynamics of a wide variety of liquid jet configurations for general liquid rocket engine injection system applications. This model includes physical models for droplet atomization, breakup/coalescence, evaporation, turbulence mixing and gas-phase combustion. Benchmark validation cases for liquid rocket engine chamber combustion conditions will be performed for model validation purpose. Test cases may include shear coaxial, swirl coaxial and impinging injection systems with combinations LOXIH2 or LOXISP-1 propellant injector elements used in rocket engine designs. As a final goal of this project, a well tested parallel CFD performance methodology together with a user's operation description in a final technical report will be reported at the end of the proposed research effort.
File Size	74443524
Page Count	95
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19990045901
Archival Resource Key	ark:/13960/t4qk2c012
Language	English
Publisher Date	1998-04-04
Access Restriction	Open
Subject Keyword	Computational Fluid Dynamics Manuals Evaporation Injection Liquid Propellant Rocket Engines Grid Generation Mathematics Atomizing Parallel Processing Computers User Manuals Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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