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THE COMPUTATIONS OF AERODYNAMIC COEFFICIENTS AND HEAT TRANSFER RATE FOR SATELLITES BY THE NOCILLA MODE

Wang Zhonglian (Beijing Institute of Spacecraft System Engineering)   

  • Published:1987-08-25

Abstract: In this paper the total aerodynamic coefficients and heat transfer rate over the satellites in orbit are calculated by the Nocilla particle-surface interaction mode and the detail calculating formula and one example are given.