Improved k-ω-γ model for crossflow-induced transition prediction in hypersonic flow
L Zhou, R Li, Z Hao, DI Zaripov, C Yan - … Journal of Heat and Mass Transfer, 2017 - Elsevier
Accurate prediction of boundary layer transition is extremely important for the aerodynamic
and aerothermodynamic design of a hypersonic vehicle. Crossflow instability plays a crucial …
and aerothermodynamic design of a hypersonic vehicle. Crossflow instability plays a crucial …
[HTML][HTML] 高超声速边界层转捩研究现状与趋势
杨武兵， 沈清， 朱德华， 禹旻， 刘智勇 - 空气动力学学报, 2018 - html.rhhz.net
在过去15 年间, 随着高超声速技术快速发展, 边界层转捩也得到了更加广泛和深入的研究.
人们对流向行波失稳, 横流失稳, Görtler 涡失稳等转捩机理取得了较深刻认识 …
人们对流向行波失稳, 横流失稳, Görtler 涡失稳等转捩机理取得了较深刻认识 …
Boundary layer transition and linear modal instabilities of hypersonic flow over a lifting body
X Chen, S Dong, G Tu, X Yuan, J Chen - Journal of Fluid Mechanics, 2022 - cambridge.org
Boundary layer transition over a lifting body of 1.6 m length at. The model geometry is the
same as the Hypersonic Transition Research Vehicle designed by the China Aerodynamics …
same as the Hypersonic Transition Research Vehicle designed by the China Aerodynamics …
Quiet tunnel measurements of HIFiRE-5 boundary-layer transition
TJ Juliano, MP Borg, SP Schneider - AIAA Journal, 2015 - arc.aiaa.org
The Hypersonic International Flight Research Experimentation (HIFiRE) program is a
hypersonic flight test program executed by the Air Force Research Laboratory and …
hypersonic flight test program executed by the Air Force Research Laboratory and …
Linear modal instabilities of hypersonic flow over an elliptic cone
Steady laminar flow over a rounded-tip. The flow conditions are selected to match the
planned flight of the Hypersonic Flight Research Experimentation HIFiRE-5 test geometry at …
planned flight of the Hypersonic Flight Research Experimentation HIFiRE-5 test geometry at …
Direct simulation of hypersonic crossflow instability on an elliptic cone
DJ Dinzl, GV Candler - AIAA journal, 2017 - arc.aiaa.org
Direct numerical simulation is performed on a 38.1% scale Hypersonic International Flight
Research Experimentation Program Flight 5 forebody to study stationary crossflow …
Research Experimentation Program Flight 5 forebody to study stationary crossflow …
Traveling crossflow instability for the HIFiRE-5 elliptic cone
A 38.1%-scale model of the Hypersonic International Flight Research Experimentation
Program's Flight Five 2: 1 elliptic cone flight vehicle was used to investigate the traveling …
Program's Flight Five 2: 1 elliptic cone flight vehicle was used to investigate the traveling …
Implementation of self-aligned focusing Schlieren for hypersonic boundary layer measurements
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 …
schlieren (SAFS) apparatus based on a recently published design is implemented for the …
Stability analysis for HIFiRE experiments
The HIFiRE-1 flight experiment provided a valuable database pertaining to boundary layer
transition over a 7-degree half-angle, circular cone model from supersonic to hypersonic …
transition over a 7-degree half-angle, circular cone model from supersonic to hypersonic …
HIFiRE-5b heat flux and boundary-layer transition
Hypersonic International Flight Research Experimentation (HIFiRE)-5 is a hypersonic flight-
test experiment designed to investigate the aerothermodynamics of a three-dimensional …
test experiment designed to investigate the aerothermodynamics of a three-dimensional …