[HTML][HTML] 高超声速边界层转捩研究现状与发展趋势
陈坚强， 涂国华， 张毅锋， 徐国亮， 袁先旭， 陈诚 - 2017 - html.rhhz.net
高超声速飞行器边界层容易经历层流/湍流转捩, 层流流动和湍流流动在摩擦阻力, 热交换,
噪声和掺混等方面有巨大差别, 转捩问题已成为制约高超声速技术突破的基础科学问题之一 …
噪声和掺混等方面有巨大差别, 转捩问题已成为制约高超声速技术突破的基础科学问题之一 …
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 …
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 …
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 …