Verification, calibration, and validation of stall delay models using NREL phase VI and MEXICO data

Author:

Ouakki Yassine1ORCID,Arbaoui Abdelaziz1ORCID

Affiliation:

1. INSCM Team, LM2I, National School of Arts and Crafts (ENSAM), Moulay Ismail University of Meknès, BP 4024 Meknes, Morocco

Abstract

An accurate estimation of rotational effects is critical during the preliminary design of wind turbines. For this purpose, different stall delay models were developed based on the centrifugal pumping mechanism. However, their generality is not yet thoroughly evaluated. In this work, we investigated the causal relationship between the radial flow, the pressure reduction, and forces augmentation. Three stall delay models, which represent different solutions of the centrifugal pumping mechanism, were verified and modified to accurately predict the radial flow, the pressure coefficient, and normal and tangential force coefficients. Then, the three modified stall delay models were calibrated using radial flow data available from the literature. Finally, they were validated against the experimental data of the NREL phase VI and MEXICO rotors. The results showed that the centrifugal pumping produces a small chordwise pressure gradient in the separated boundary layer, which produces a small augmentation in the normal and tangential force coefficients. In contrast, the measured pressure coefficient and the normal and tangential force coefficients showed a large augmentation compared to the three modified stall delay models. Consequently, the lack of generality of current stall delay models is mainly due to the centrifugal pumping assumption. Furthermore, the verification and calibration of these stall delay models allowed us to isolate large errors in the model's output due to the model's assumptions. Thus, the importance of a rigorous verification and calibration before performing the validation.

Publisher

AIP Publishing

Subject

Renewable Energy, Sustainability and the Environment

Reference61 articles.

1. Multi-objective optimization of a thick blade root airfoil to improve the energy production of large wind turbines

2. An analytical model for airfoil aerodynamic characteristics over the entire 360° angle of attack range

3. Accuracy of the aerodynamic performance of wind turbines using vortex core models in the free vortex wake method

4. Y. Kim , “ Computational airfoil optimization for the improvement of the performance of horizontal axis wind turbines (HAWT) with a 3D model,” Ph.D. thesis

5. Y. Kim [ Friedrich-Alexander-Universität Erlangen-Nürnberg (FAU), 2020].

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Detailed Analytical Solution for Performance Prediction of Ideal Horizontal Wind Turbines;2024 4th International Conference on Innovative Research in Applied Science, Engineering and Technology (IRASET);2024-05-16

2. On the influence of twist and taper of HAWT blades on the rotational augmentation phenomenon: the NREL Phase VI – Phase II comparison;Journal of Physics: Conference Series;2023-12-01

3. Improved order of magnitude estimate of rotational effects on HAWTs;Results in Engineering;2023-09

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3