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Design of high-reynolds-number flat-plate experiments in the ntf
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Saric, William S. |
| Copyright Year | 1988 |
| Description | The design of an experiment to measure skin friction and turbulent boundary layer characteristics at Reynolds numbers exceeding 1 x 10 to the 9th is described. The experiment will be conducted in a zero-pressure-gradient flow on a flat plate in the National Transonic Facility (NTF). The development of computational codes to analyze the aerodynamic loads and the blockage is documented. Novel instrumentation techniques and models, designed to operate in cryogenic environments, are presented. Special problems associated with aerodynamic loads, surface finish, and hot-wire anemometers are discussed. |
| File Size | 826954 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890004040 |
| Archival Resource Key | ark:/13960/t5n924v6p |
| Language | English |
| Publisher Date | 1988-12-19 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics High Reynolds Number Turbulence Flat Plates Computational Fluid Dynamics Skin Friction Transonic Wind Tunnels Hot-wire Anemometers Design Analysis Surface Finishing Pressure Gradients Coding Aerodynamic Loads Boundary Layer Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |