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Host combustion r and t overview
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gaugler, Raymond E. |
| Copyright Year | 1986 |
| Description | The overall objective of the Turbine Engine Hot Section Technology Combustion Project was to develop and verify improved and more accurate numerical analysis methods for increasing the ability to design with confidence combustion systems for advanced aircraft gas turbine engines. The objective was approached from two directions: computational and experimental. On the computational side, the approach was to first assess and evaluate existing combustor aerothermal analysis models. On the experimental side, three types of experiments are identified; first, fundamental experiments directed toward improved understanding of the flow physics and chemistry; second, experiments run to provide data for the empirical modeling of complex phenomena; and third, benchmark experiments for computer code validation. |
| File Size | 171100 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890003508 |
| Archival Resource Key | ark:/13960/t5hb4105m |
| Language | English |
| Publisher Date | 1986-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Numerical Analysis Turbulent Flow Engine Design Gas Turbine Engines General Overviews Computerized Simulation Aircraft Engines Combustion Chambers Recirculative Fluid Flow Aerothermodynamics Viscous Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
