Design And Calibration Of A Total Temperature Probe For Use At Supersonic Speeds
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| Author | : David L. Goldstein |
| Publisher | : |
| Total Pages | : 17 |
| Release | : 1949 |
| Genre | : Probes (Electronic instruments) |
| ISBN | : |
Download Design and Calibration of a Total-temperature Probe for Use at Supersonic Speeds Book in PDF, Epub and Kindle
The results of a study of the factors involved in the design of total-temperature probes for use at supersonic speeds have been applied to the design of an instrument to be used in wind-tunnel calibrations. Tests of the probe showed that the calibration factor required in the conversion of the measured temperature to the true total temperature was 0.992 pluse or minus 0.002 for a range of Mach numbers between 1.36 and 2.01. The calibration factor was insensitive to angles of inclination relative to the air stream up to 9 degrees at a Mach number of 1.50.
| Author | : EVA M. WINKLER |
| Publisher | : |
| Total Pages | : 2 |
| Release | : 1953 |
| Genre | : |
| ISBN | : |
Download Design and Calibration of Stagnation Temperature Probes for Use at High Supersonic Speeds and Elevated Temperatures Book in PDF, Epub and Kindle
| Author | : Robert A. Langworthy |
| Publisher | : |
| Total Pages | : 50 |
| Release | : 1962 |
| Genre | : Boundary layer |
| ISBN | : |
Download The design and calibration of a total temperature probe for use in a Mach 5 turbulent boundary layer with heat transfer Book in PDF, Epub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 280 |
| Release | : 1949 |
| Genre | : Aeronautics |
| ISBN | : |
Download Technical Note - National Advisory Committee for Aeronautics Book in PDF, Epub and Kindle
| Author | : R. L. P. Voisinet |
| Publisher | : |
| Total Pages | : 88 |
| Release | : 1974 |
| Genre | : Fluid mechanics |
| ISBN | : |
Download Comparative Measurements of Total Temperature in a Supersonic Turbulent Boundary Layer Using a Conical Equilibrium and Combined Temperature-pressure Probe Book in PDF, Epub and Kindle
The predominant probes used for measuring total temperature in a compressible boundary-layer flow are described. The results of a direct comparison between two of these probes, the conical equilibrium temperature probe (Danberg probe) and the combined temperature-pressure probe of the DFVLR-AVA, are presented. The comparison was made by testing the probes simultaneously in the nozzle-wall turbulent boundary-layer flow of the NOL Boundary Layer Channel at zero and moderate heat-transfer conditions...
| Author | : Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md |
| Publisher | : |
| Total Pages | : 516 |
| Release | : 1961 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
Download Handbook of Supersonic Aerodynamics Book in PDF, Epub and Kindle
| Author | : R. J. Volluz |
| Publisher | : |
| Total Pages | : 512 |
| Release | : 1961 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
Download Handbook of Supersonic Aerodynamics Book in PDF, Epub and Kindle
| Author | : M. A. Shadday |
| Publisher | : |
| Total Pages | : 4 |
| Release | : 1978 |
| Genre | : |
| ISBN | : |
Download Total Temperature Probe Calibration in Supersonic Rarefied Flows Book in PDF, Epub and Kindle
| Author | : M. O. Varner |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1976 |
| Genre | : Probes (Electronic instruments) |
| ISBN | : |
Download Corrections to Single-shielded Total Temperature Probes in Subsonic, Supersonic, and Hypersonic Flow Book in PDF, Epub and Kindle
A new total temperature measurement correction is developed for the single-shielded type of probe. This method is based on a detailed analysis of the coupled heat transfer-viscous flow region existing within the probe. The correction is valid for all flow-field conditions and requires probe calibration data only in the free stream where flow properties are known. Total temperature measurements on the windward ray of a 4-deg sharp cone at Mach 10 in AEDC Hypersonic Tunnel (C) are used in conjunction with corresponding theoretical predictions to substantiate the present analysis. The new approach appears to be a significant improvement over present methods. (Author).
| Author | : |
| Publisher | : |
| Total Pages | : 694 |
| Release | : 1949 |
| Genre | : Science |
| ISBN | : |
Download Technical Information Pilot Book in PDF, Epub and Kindle
