scispace - formally typeset
C

Chao Li

Researcher at Hunan University of Science and Technology

Publications -  6
Citations -  52

Chao Li is an academic researcher from Hunan University of Science and Technology. The author has contributed to research in topics: Wind tunnel & Aerodynamics. The author has an hindex of 2, co-authored 4 publications receiving 17 citations.

Papers
More filters
Journal ArticleDOI

Aerodynamic performance of CAARC standard tall building model by various corner chamfers

TL;DR: In this paper, the effects of corner chamfers on the aerodynamic performance of tall buildings were investigated and correlation factors for base moment coefficients and power spectral densities were proposed.
Journal ArticleDOI

Research on the characteristics of wind pressures on L-shaped tall buildings

TL;DR: In this article, eight L-shaped rigid models with different geometric dimensions were tested at four typical terrain categories in a boundary wind tunnel to investigate the characteristics of wind pressures on L-shapes.
Journal ArticleDOI

Reduction of wind loads on rectangular tall buildings with different taper ratios

TL;DR: In this paper, the influence of different taper ratios on wind loads reduction on rectangular tall buildings is explored and correlation factors for base moment coefficients and their power spectral densities concerning the effects of different Taper ratios are provided.
Journal ArticleDOI

Refined Mathematical Models for Across-Wind Loads of Rectangular Tall Buildings with Aerodynamic Modifications

TL;DR: In this paper, the authors systematically study the across-wind loads of rectangular-shaped tall buildings with aerodynamic modifications and propose refined mathematic models accordingly, taking into account the aerodynamic properties of the buildings.
Journal ArticleDOI

A Modified RANS Model for Drag Prediction of Practical Configuration with Riblets and Experimental Validation

Chao Li, +3 more
- 28 Feb 2022 - 
TL;DR: In this article , the k-ω SST turbulence model with Rotation and Curvature correction (SST-RC) is modified to predict the drag of practical aerodynamic configurations mounted with drag-reducing riblets.