Accurate prediction of boundary-layer transition is critical to optimizing the performance of
hypersonic vehicles. Boundary-layer transition can increase aerodynamic heating by a …

View Video Presentation: https://doi. org/10.2514/6.2023-2438. vid A self-aligned focusing
schlieren (SAFS) apparatus based on a recently published design is implemented for the …

Boundary-layer stability and laminar-to-turbulent transition are examined on the Boundary
Layer Transition flight-test vehicle using predicted flow conditions at ascent and descent …

The transition of a laminar to turbulent boundary layer for a high speed vehicles plays an
important role in their design due to comparatively higher heat flux and skin friction drag …

Hypersonic International Flight Research Experimentation (HIFiRE)-5 is a hypersonic flight-
test experiment designed to investigate the aerothermodynamics of a three-dimensional …

Non-modal linear stability analysis results are presented for hypersonic flow over an elliptic
cone with an aspect ratio of two at zero angle of attack, completing earlier modal instability …

考虑气动, 轨迹, 约束, 指标间的耦合关系, 以多高超声速飞行器同时到达为目标建立了协同规划
模型; 设计了一种自动满足终端约束的全新滑翔飞行剖面, 减少了规划算法需要处理的约束数量; …

The Hypersonic International Flight Research and Experimentation (HIFiRE) 5 flight
experiment by the Air Force Research Laboratories and Australian Defense Science and …

The principal goal of the Hypersonic International Flight Research Experimentation (HIFiRE)
flight 5 is to measure hypersonic boundary-layer transition on a three-dimensional body …

The Hypersonic International Flight Research Experimentation (HIFiRE) program is a
hypersonic flight-test program executed by the US Air Force Research Laboratory and the …