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  • 1
    Publication Date: 2019-06-28
    Type: NACA-RM-A58D17a
    Format: application/pdf
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  • 2
    Publication Date: 2019-07-13
    Description: The vaporization of graphite under intense laser radiation is considered both theoretically and experimentally. Under intense radiation, the mass-loss rate can be high enough to cause the flow in the laser plume to be supersonic. Under these conditions, the vaporization process is coupled to the plume gasdynamics. Experimental results are presented for surface temperatures of 3985 to 4555 K and mass-loss rates from 0.52 to 27.0 g/sq cm sec. The data are used to determine the vapor pressure of graphite in a range of 2 to 11 atm, and the results are shown to be in good agreement with the JANAF vapor pressure curve, if the vaporization coefficients are unity. The assumption of unity vaporization coefficients is shown to be reasonable by a comparison of the present results with other recent vapor pressure results for graphite.
    Keywords: Nonmetallic Materials
    Type: AIAA Paper 76-166 , Progress in Astronautics and Aeronautics: Thermophysics of Spacecraft and Outer Planet Entry Probes; 56; 405-422|14th Aerospace Sciences Meeting; Jan 26, 1976 - Jan 28, 1976; Washington, DC; United States
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  • 3
    Publication Date: 2019-07-13
    Description: Results of an extensive experimental program on the ablation of ATJ graphite in air at surface pressures of 0.3 to 4.4 atm and surface temperatures of 2570 to 4030 K are presented. The measured mass-loss rates are correlated with surface temperature, pressure, and effective nose radius. The results are compared with several equilibrium thermochemical ablation theories which differ basically in the chemical species that are considered and in the thermodynamic properties assigned to these species. All the theories predict about the same mass-loss rate in the diffusion-controlled oxidation regime and are in good agreement with the experimental results. At higher temperatures, however, the experimental and theoretical results do not agree. At temperatures above 3700 K, the experimental mass-loss rate becomes independent of pressure and an exponential function of temperature. A comparison of the high-temperature results with the theories indicates that all the theories, except the one based on the thermodynamic properties from the JANAF tables, are invalid because they overpredict the mass-loss rate. On the other hand, the theory based on the JANAF properties underpredicts the measured mass-loss rate by a factor of three at 4000 K. At least a portion of this difference between experiment and theory is attributed to particulate mass loss which is visually observed.
    Keywords: Nonmetallic Materials
    Type: NASA-TM-112782 , NAS 1.15:112782 , AIAA Paper 71-418 , AIAA Journal; 11; 2; 216-222|Thermophysics; Apr 26, 1971 - Apr 28, 1971; Tullahoma, TN; United States
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  • 4
    Publication Date: 2019-08-16
    Description: An idealized axisymmetric, all-internal compression inlet was designed for a Mach number of 3.75. The objective of the design was to obtain a steady, one-dimensional transonic flow and a high over-all total pressure recovery. Boundary-layer removal was employed in the vicinity of the inflection point of the supersonic contour. Static and total-pressure fluctuations were measured in the transonic flow region. A total pressure recovery of about 90 percent was obtained with a boundary-layer-removal mass flow rate of 15 percent of the inlet mass flow rate. The accompanying root-mean-square total pressure fluctuation in the throat region was only 1 percent of the free stream total pressure. The test Mach number was 3.80 and the Reynolds number based on inlet diameter was 2.63 x 10(exp 6).
    Keywords: Fluid Mechanics and Thermodynamics
    Type: NASA-TN-D-854 , A-405
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