Aerospaceplanes; Air breathing engines; Boundary layer; Air Force; Aircraft; Coding; Compression; Computations; Finite difference theory; Generators; Growth(General); Hypersonic characteristics; Hypersonic velocity; Injection; Inlets; Mathematical models; Orbits; Profiles; Propulsion systems; Regions; Runways; Supersonic flow; Surfaces; Test and evaluation; Theses; Thickness; Two dimensional; Velocity; Hypersonic flight; Hypersonic aircraft; Bleed systems; Ingestion(Engines); Boundary value problems; Intake; Forebody; Precompression Surfaces;
机译:超声波湍流边界层空气计算湍流建模的改进
机译:在计算风能工程中为中性平衡大气边界层建模的新入流边界条件
机译:用计算流体力学评估燃气轮机加力扩散器的湍流边界层建模方法
机译:具有CVDEV模型的超声缺陷边界层计算
机译:用于火箭发动机测试的质量增加高度模拟的简单一维可压缩流分析。
机译:使用边界层提高耳蜗模型的计算效率
机译:Baldwin-Lomax湍流模型在二维,不稳定和可压缩边界层中的进气口分离和不分离的评估和应用