Thermophysics of Atmospheric EntryThomas E. Horton |
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Contents
Numerical Calculation of Gaseous Transport Properties | 3 |
Transport Properties for a Mixture of the Ablation Products C C₂ | 17 |
Transport Properties Associated with Entry into the Atmosphere | 37 |
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ablation aerocapture altitude analysis angle of attack approximation assumed atmosphere Ballute blunt body boundary boundary-layer calculated carbon catalytic Chemical coefficient comparison composition computed conductivity cone configuration constant convective cool core correlation density determined developed distribution effect energy engineering entry environment equations experiment experimental flight flow flowfield force freestream given heat flux Heat Transfer heat-shield heat-transfer heating rates increase injection integrals interaction Journal laminar layer loss mass material measurements method mission mixture NASA normal nose nosetip obtained Orbiter parameters peak Physics potential predicted present pressure probe radiation radiative heating range region shape shock shock layer shown in Fig shows simulation solutions Space species stagnation point surface Table temperature thermal thickness tion trajectory transition trip turbulent values vehicle viscosity wall