Assessment of laminar-turbulent transition models for Hypersonic Inflatable Aerodynamic Decelerator aeroshell in convection heat transfer

•Assessment of three tansition models for simulations of HIAD is conducted.•Crossflow effects on performances of transition models for HIAD are analyzed.•Crossflow instability mode and the first disturbance mode dominate the transition. Hypersonic Inflatable Aerodynamic Decelerator (HIAD) has shown...

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Veröffentlicht in:	International journal of heat and mass transfer 2019-04, Vol.132, p.825-836
Hauptverfasser:	Zhao, Yatian, Yan, Chao, Liu, Hongkang, Qin, Yupei
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aerospace industry Boundary layer transition Computational fluid dynamics Cross flow Crossflow instability Deceleration Deformation mechanisms Fluid flow Heat transfer HIAD Hypersonic Mathematical models Predictions Reynolds number Scalloping Stability analysis Survivability Thermal protection Transition model Valleys
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