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Progress in modeling hypersonic turbulent boundary layers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Zeman, Otto |
| Copyright Year | 1993 |
| Description | A good knowledge of the turbulence structure, wall heat transfer, and friction in turbulent boundary layers (TBL) at high speeds is required for the design of hypersonic air breathing airplanes and reentry space vehicles. This work reports on recent progress in the modeling of high speed TBL flows. The specific research goal described here is the development of a second order closure model for zero pressure gradient TBL's for the range of Mach numbers up to hypersonic speeds with arbitrary wall cooling requirements. |
| File Size | 617391 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940007828 |
| Archival Resource Key | ark:/13960/t71w0f47j |
| Language | English |
| Publisher Date | 1993-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Hypersonics Turbulence Hypersonic Speed Cooling Friction High Speed Turbulent Boundary Layer Reentry Vehicles Hypersonic Boundary Layer Walls Mach Number Pressure Gradients 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 |
