Computational Aerothermodynamic Design Issues for Hypersonic Vehicles
作者： Peter A. Gnoffo , K. James Weilmuenster , H. Harris Hamilton , David R. Olynick , Ethiraj Venkatapathy
DOI: 10.2514/2.3430
关键词: Multidisciplinary design optimization 、 Spacecraft design 、 Space Shuttle thermal protection system 、 Aerospace engineering 、 Context (language use) 、 Process (engineering) 、 Engineering design process 、 Hypersonic speed 、 Computational fluid dynamics 、 Engineering
摘要: … and mass ux (ablation) on a vehicle. Hypersonic ows are usually characterized by the presence of … is critical to the design of any vehicle that ies at hypersonic velocities. Fluid forces are …
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