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Fig. 9 | Advances in Aerodynamics

Fig. 9

From: Gas-kinetic unified algorithm for computable modeling of Boltzmann equation and application to aerothermodynamics for falling disintegration of uncontrolled Tiangong-No.1 spacecraft

Fig. 9

Validation of computation and experiment for aerodynamics on the two-capsule vehicle of Tiangong spacecraft (H = 62.1km, Ma = 12.79, Kn = 3.37 × 10−5). a Pressure, b Temperature, c Structural Temp. at 801s, d Normal force coefs, e Pitching moment coefs, f Pressure center position

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