[HTML][HTML] Improved local amplification factor transport equation for stationary crossflow instability in subsonic and transonic flows
XU Jiakuan, Q Lei, BAI Junqiang - Chinese Journal of Aeronautics, 2020 - Elsevier
Transition prediction is a hot research topic of fluid mechanics. For subsonic and transonic
aerodynamic flows, e N method based on Linear Stability Theory (LST) is usually adopted …
aerodynamic flows, e N method based on Linear Stability Theory (LST) is usually adopted …
Simplified stability-based transition transport modeling for unstructured computational fluid dynamics
DG François, A Krumbein, N Krimmelbein, C Grabe - Journal of Aircraft, 2023 - arc.aiaa.org
Inspired by the γ− Re θ t model framework, a new γ-based model was developed and
implemented into an unstructured Reynolds-averaged Navier–Stokes (RANS) code. The …
implemented into an unstructured Reynolds-averaged Navier–Stokes (RANS) code. The …
High-Reynolds number transitional flow simulation via parabolized stability equations with an adaptive RANS solver
The accurate prediction of transition is relevant for aerodynamic analysis and design
applications. Extending the laminar flow region over airframes is a potential way to reduce …
applications. Extending the laminar flow region over airframes is a potential way to reduce …
A CFD‐Compatible Amplification Factor Transport Equation for Oblique Tollmien‐Schlichting Waves in Supersonic Boundary Layers
JK Xu, L Qiao, J Bai - International Journal of Aerospace …, 2020 - Wiley Online Library
Boundary layer transition is a hot research topic in fluid mechanics and aerospace
engineering. In low‐speed flows, two‐dimensional Tollmien‐Schlichting (T‐S) waves always …
engineering. In low‐speed flows, two‐dimensional Tollmien‐Schlichting (T‐S) waves always …
Receptivity and Stability Theory Analysis of a Transonic Swept Wing Experiment
Y Liu, Y Liu, Z Ji, Y Wang, J Xu - Aerospace, 2023 - mdpi.com
Surface suction provides an efficient way to delay boundary layer transitions. In order to
verify the suction effects and determine the mechanism of suction control in transonic swept …
verify the suction effects and determine the mechanism of suction control in transonic swept …
An inverse design method with aerodynamic design optimization for wing glove with hybrid laminar flow control
Y Yang, J Bai, L Li, T Yang, H Wang, S Ma… - Aerospace Science and …, 2019 - Elsevier
The design of the hybrid laminar flow control (HLFC) system involves the comprehensive
design of the suction control and the profile, and it has become an urgent problem for a three …
design of the suction control and the profile, and it has become an urgent problem for a three …
Study on the Differences of Transition and Separation Characteristics Between Water and Air
D Peng, J Xiao, X Han, Y Li - International Journal of Applied …, 2022 - World Scientific
The change of flow state in the flow field significantly impacts the operational performance of
fluid machinery equipment such as aircraft or underwater vehicles, among which transition …
fluid machinery equipment such as aircraft or underwater vehicles, among which transition …
[图书][B] The Design and Validation of a UAV Propeller Intended for Extremely Low Reynolds Number Environments
B Hebert - 2020 - search.proquest.com
Mars exploraon and UAV development have both advanced significantly over the past
century, and are now being considered in tandem. Currently needed are UAV propellers that …
century, and are now being considered in tandem. Currently needed are UAV propellers that …
Propagation of Three-Dimensional Disturbances Over Finite Wings
E Badcock, S Mughal - AIAA AVIATION FORUM AND ASCEND 2024, 2024 - arc.aiaa.org
This study presents advancements to a laminar-to-turbulent transition prediction technique
based on the linear PSE3D framework. This method models disturbance propagation …
based on the linear PSE3D framework. This method models disturbance propagation …
Aerodynamic Shape Optimization and Modeling for Flows Including Transition to Turbulence Effects
GL Olichevis Halila - 2020 - deepblue.lib.umich.edu
In airplane design, engineers aim to reduce drag as much as possible, while respecting
aerodynamic, structural, and budgetary constraints, leading to reduced operational costs …
aerodynamic, structural, and budgetary constraints, leading to reduced operational costs …