Computer Science – Performance
Scientific paper
May 1979
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979jatp...41..453r&link_type=abstract
Journal of Atmospheric and Terrestrial Physics, vol. 41, May 1979, p. 453-473.
Computer Science
Performance
49
Ablation, Hypersonic Reentry, Mathematical Models, Meteorites, Performance Prediction, Aerodynamic Drag, Approximation, Computerized Simulation, Convective Heat Transfer, Heat Transfer Coefficients, Photogrammetry, Radiative Heat Transfer, Turbulent Boundary Layer
Scientific paper
A single-body one-dimensional ablation model has been developed in order to predict the entry behavior of large meteorites during their hypersonic drag interaction with the earth's atmosphere. The entry predictions are compared with multistation photographic data. Typical results indicate that the ablation parameter, sigma, approximately equals 0.02-0.03 sq sec/sq km in the vicinity of the peak ablation altitude.
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