Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: The role of quiet tunnels
SP Schneider - Progress in Aerospace Sciences, 2015 - Elsevier
For more than half a century, researchers have been aware that freestream fluctuations have
an important effect on laminar-turbulent transition. A century of effort has also been devoted …
an important effect on laminar-turbulent transition. A century of effort has also been devoted …
[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 …
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 …
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 …
HIFiRE-5 flight test results
TJ Juliano, D Adamczak, RL Kimmel - Journal of Spacecraft and …, 2015 - arc.aiaa.org
The Hypersonic International Flight Research Experimentation (HIFiRE-5) is a hypersonic
flight test vehicle designed to investigate the aerothermodynamics of a three-dimensional …
flight test vehicle designed to investigate the aerothermodynamics of a three-dimensional …
Streak instabilities on HIFiRE-5 elliptic cone
MM Choudhari, F Li, P Paredes - AIAA Scitech 2020 Forum, 2020 - arc.aiaa.org
The Hypersonic International Flight Research and Experimentation (HIFiRE) 5 flight
experiment by the Air Force Research Laboratories and Australian Defense Science and …
experiment by the Air Force Research Laboratories and Australian Defense Science and …
Identification of traveling crossflow waves under real hypersonic flight conditions
B Wan, G Tu, X Yuan, J Chen, Y Zhang - Physics of Fluids, 2021 - pubs.aip.org
Understanding crossflow instabilities in three-dimensional boundary layers triggered by
either traveling crossflow waves or stationary crossflow vortices is of great importance for …
either traveling crossflow waves or stationary crossflow vortices is of great importance for …
Verification and validation issues in hypersonic stability and transition prediction
HL Reed, E Perez, J Kuehl, T Kocian… - Journal of Spacecraft and …, 2015 - arc.aiaa.org
The development, validation, and introduction of physics-based approaches for stability and
transition prediction will lead to smaller and more manageable uncertainties in the design of …
transition prediction will lead to smaller and more manageable uncertainties in the design of …