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Direct measurements and analysis of skin friction and cooling downstream of multiple flush-slot injection into a turbulent mach 6 boundary layer
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Howard, F. G. Strokowski, A. J. |
| Copyright Year | 1978 |
| Description | Experiments were conducted to determine the reduction in surface skin friction and the effectiveness of surface cooling downstream of one to four successive flush slots injecting cold air at an angle of 10 deg into a turbulent Mach 6 boundary layer. Data were obtained by direct measurement of surface shear and equilibrium temperatures, respectively. Increasing the number of slots decreased the skin friction, but the incremental improvement in skin-friction reduction decreased as the number of slots was increased. Cooling effectiveness was found to improve, for a given total mass injection, as the number of slots was increased from one to four. Comparison with previously reported step-slot data, however, indicated that step slots with tangential injection are more effective for both reducing skin friction and cooling than the present flush-slot configuration. Finite-difference predictions are in reasonable agreement with skin-friction data and with boundary-layer profile data. |
| File Size | 6696795 |
| Page Count | 114 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780025442 |
| Archival Resource Key | ark:/13960/t14n4078c |
| Language | English |
| Publisher Date | 1978-10-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Friction Reduction Surface Cooling Cold Gas Drag Reduction Skin Friction Finite Difference Theory Turbulent Boundary Layer Data Processing Friction Measurement Film Cooling Fluid Injection Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |