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Heat transfer in rocket combustion chambers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Farmer, R. Cheng, G. Anderson, P. |
| Copyright Year | 1993 |
| Description | Complexities of liquid rocket engine heat transfer which involve the injector faceplate and film cooled walls are being investigated by computational analysis. A conjugate heat transfer analysis was used to describe localized heating phenomena associated with particular injector configurations and film coolant flows. These components were analyzed, and the analyses verified when appropriate test data were available. The component analyses are being synthesized into an overall flowfield/heat transfer model. A Navier-Stokes flow solver, the FDNS code, was used to make the analyses. Particular attention was given to the representation of the thermodynamic properties of the fluid streams. Unit flow models of specific coaxial injector elements have been developed and are being used to describe the flame structure near the injector faceplate. |
| File Size | 132671 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940018578 |
| Archival Resource Key | ark:/13960/t0ps2q208 |
| Language | English |
| Publisher Date | 1993-11-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Injectors Computational Fluid Dynamics Flow Characteristics Fuel Flow Temperature Profiles Navier-stokes Equation Engine Coolants Liquid Oxygen Flow Distribution Space Shuttle Main Engine Mathematical Models Film Cooling Liquid Propellant Rocket Engines Thermodynamic Properties Fuel Injection Combustion Chambers Heat Transfer 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 |
