Computational study of hypersonic rarefied gas flow over re-entry vehicles using the second-order Boltzmann-Curtiss constitutive model

• المؤلفون الرئيسيون: Chourushi, Tushar, Singh, Satyvir, Sreekala, Vishnu Asokakumar, Myong, Rho Shin
• مؤلفون آخرون: School of Physical and Mathematical Sciences
• التنسيق: مقال
• اللغة: English
• منشور في: 2022
• الموضوعات: Engineering::Mechanical engineering::Fluid mechanics; Hypersonic Re-Entry Vehicles; Rarefied Gas Flows
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/156103
• المؤسسة: Nanyang Technological University

The aerothermodynamics of re-entry vehicles vary significantly upon re-entry, descent, and landing, because of the drastic changes in atmospheric density and velocity. In highly rarefied regimes, the conventional Navier-Stokes-Fourier equations may not provide an accurate prediction of aerothermod...