Measurements Of Upstream History Effects In Compressible Turbulent Boundary Layers
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| Author | : David F. Gates |
| Publisher | : |
| Total Pages | : 124 |
| Release | : 1973 |
| Genre | : Supersonic nozzles |
| ISBN | : |
The report describes an experimental study of compressible turbulent boundary layers for which the upstream history was systematically varied. A series of experiments was conducted using both a supersonic half nozzle and a conventional flat plate for which the nozzle throat and flat plate leading edge can be temperature controlled. The supersonic nozzle provided a favorable upstream pressure gradient together with a controlled thermal history at the throat. The flat plate provided upstream temperature control with no pressure history. Velocity and temperature profile and heat-transfer measurements were made in a downstream region of zero-pressure-gradient and constant wall temperature. (Modified author abstract).
| Author | : David F. Gates |
| Publisher | : |
| Total Pages | : 101 |
| Release | : 1973 |
| Genre | : |
| ISBN | : |
The report describes an experimental study of compressible turbulent boundary layers for which the upstream history was systematically varied. A series of experiments was conducted using both a supersonic half nozzle and a conventional flat plate for which the nozzle throat and flat plate leading edge can be temperature controlled. The supersonic nozzle provided a favorable upstream pressure gradient together with a controlled thermal history at the throat. The flat plate provided upstream temperature control with no pressure history. Velocity and temperature profile and heat-transfer measurements were made in a downstream region of zero-pressure-gradient and constant wall temperature. (Modified author abstract).
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 814 |
| Release | : 1978 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 580 |
| Release | : 1969 |
| Genre | : Compressibility |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 826 |
| Release | : 1978 |
| Genre | : Astronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 768 |
| Release | : 1994 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 1000 |
| Release | : 1974 |
| Genre | : Research |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 344 |
| Release | : 1979 |
| Genre | : Aerodynamics |
| ISBN | : |
| Author | : Edwin J. Saltzman |
| Publisher | : |
| Total Pages | : 52 |
| Release | : 1970 |
| Genre | : Skin friction (Aerodynamics) |
| ISBN | : |
| Author | : Robert L. P. Voisinet |
| Publisher | : |
| Total Pages | : 144 |
| Release | : 1973 |
| Genre | : Fluid mechanics |
| ISBN | : |
The results of a detailed experimental investigation of the compressible turbulent boundary layer in a favorable-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall at momentum thickness Reynolds numbers from 6,700 to 56,000 and at three wall-to-adiabatic-wall temperature ratios. An attempt was made to hold values of Clauser's pressure-gradient parameter constant. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. (Modified author abstract).
