Fast pressure-sensitive paint for understanding complex flows: from regular to harsh environments

D Peng, Y Liu - Experiments in Fluids, 2020 - Springer
This review summarizes state-of-the-art knowledge on fast-responding pressure-sensitive
paint (fast PSP), which has evolved into a powerful experimental tool for studying complex …

[HTML][HTML] 风能利用中的空气动力学研究进展Ⅰ: 风力机气动特性

王同光, 田琳琳, 钟伟, 王珑, 朱呈勇 - 空气动力学学报, 2022 - html.rhhz.net
随着世界各国纲领性行业政策的积极制定, 风电行业将继续高速发展. 风电机组大型化(达到多兆
瓦级甚至十兆瓦级), 海洋化(从陆地扩展至海上), 智能化(辅以智能化结构, 材料和控制策略) …

[图书][B] Pressure and temperature sensitive paints

T Liu, JP Sullivan, K Asai, C Klein, Y Egami - 2005 - Springer
The first edition of the book “Pressure and Temperature Sensitive Paints” published by
Springer in 2005 summarizes the early development of pressure-and temperature-sensitive …

[HTML][HTML] Data-driven approach for noise reduction in pressure-sensitive paint data based on modal expansion and time-series data at optimally placed points

T Inoue, Y Matsuda, T Ikami, T Nonomura, Y Egami… - Physics of …, 2021 - pubs.aip.org
We propose a noise reduction method for unsteady pressure-sensitive paint (PSP) data
based on modal expansion, the coefficients of which are determined from time-series data at …

Active circulation control on the blunt trailing edge wind turbine airfoil

HY Xu, CL Qiao, HQ Yang, ZY Ye - AIAA journal, 2018 - arc.aiaa.org
Active circulation control on a thick blunt trailing edge wind turbine airfoil is proposed and
numerically investigated by solving Reynolds-averaged Navier–Stokes equations along with …

Parametric investigation of stall cell formation on a NACA 0015 airfoil

H Dell'Orso, M Amitay - AIAA Journal, 2018 - arc.aiaa.org
An experimental parametric exploration of stall cells on a NACA 0015 airfoil with aspect ratio
aspect ratio= 4 was conducted. First, flowfield measurements were performed using …

Dynamic stall characteristics of unswept pitching wing

AH Ullah, C Fabijanic, J Estevadeordal - Experimental Thermal and Fluid …, 2024 - Elsevier
An experimental investigation of dynamic stall on upswept pitching wing was conducted
using Particle Image Velocimetry (PIV) and Pressure Sensitive Paint (PSP) techniques. The …

Vortex formation on surging aerofoils with application to reverse flow modelling

PB Kirk, AR Jones - Journal of fluid mechanics, 2019 - cambridge.org
The leading-edge vortex (LEV) is a powerful unsteady flow structure that can result in
significant unsteady loads on lifting blades and wings. Using force, surface pressure and …

[HTML][HTML] Nonembedded measurement method based on amplitude correction for unsteady surface pressure estimation in a high-subsonic compressor cascade

R Li, S Lin, N Ge, L Gao - Measurement, 2023 - Elsevier
Unsteady surface pressure (USP) is a crucial physical quantity for studying blade loads and
boundary layer flow. However, the unique characteristics of high-load compressor cascades …

Experimental investigation of a pitch-oscillating wind turbine airfoil with vortex generators

S Li, L Zhang, J Xu, K Yang, J Song… - Journal of Renewable and …, 2020 - pubs.aip.org
The inflow shear and turbulence, tilt or yaw misalignment, and tower passage lead to
dynamic stall on turbine blades. The effects of vortex generators (VGs) on the aerodynamic …