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- W3180562771 abstract "<p indent=0mm>The high-speed circumlunar return and reentry capsule has a reentry velocity of close to 11 km/s, and it uses a skip reentry trajectory in the Earth’s atmosphere. Therefore, the chemical non-equilibrium effect of the flow field around the capsule during its reentry is more serious and complex than is that of LEO capsules. This paper uses chemical non-equilibrium models with more than seven components to calculate and analyze the mechanism and rule of chemical non-equilibrium effects on the aerodynamic characteristics of the high-speed reentry capsule at the altitude of 60–80 km. The numerical method and boundary conditions for solving the aerodynamic characteristics of the high-speed circumlunar return and reentry capsule at mid-high altitude are then discussed. Finally, the aerodynamic parameters obtained from the circumlunar reentry flight are compared with the calculated data of the chemical non-equilibrium method established by the author, confirming that the prediction error of the trim angle of attack is less than 0.7°, and the prediction accuracy of the trim lift-drag ratio is better than 2.5%. The method established in this paper is proven to be both effective and accurate in predicting the mid-high altitude aerodynamic characteristics of the high-speed circumlunar return and reentry capsule." @default.
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- W3180562771 date "2021-07-01" @default.
- W3180562771 modified "2023-10-16" @default.
- W3180562771 title "Prediction and flight verification of chemical non-equilibrium aerodynamic characteristics of the high-speed circumlunar return and reentry capsule" @default.
- W3180562771 doi "https://doi.org/10.1360/sst-2021-0103" @default.
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