首页> 外文OA文献 >Yaw angle effect on the aerodynamic performance of hatchback vehicle fitted with wing spoiler

【2h】

Yaw angle effect on the aerodynamic performance of hatchback vehicle fitted with wing spoiler

机译：横出角度对装有机翼扰流器的车厢空气动力学性能的影响

代理获取

本网站仅为用户提供外文OA文献查询和代理获取服务，本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文，但由于OA文献来源多样且变更频繁，仍可能出现获取不到、文献不完整或与标题不符等情况，如果获取不到我们将提供退款服务。请知悉。

页面导航

著录项
引文网络
相似文献
相关主题

著录项

作者
Kwang-Yhee Chin; See-Yuan Cheng; Shuhaimi Mansor;
展开▼
作者单位

展开▼
年度 2019
总页数
原文格式 PDF
正文语种
中图分类

相似文献

外文文献
中文文献
专利

1. Experimental study of yaw angle effect on the aerodynamic characteristics of a road vehicle fitted with a rear spoiler [J] . Cheng See-Yuan, Chin Kwang-Yhee, Mansor Shuhaimi, Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 2019,第期

机译：偏航角对后扰晶的公路车辆空气动力学特性的实验研究
2. Effect of Spoiler Angle on the Aerodynamic Performance of Hatchback Model [J] . Cheng See Yuan, Shuhaimi Mansor, Mohd Azman Abdullah International Journal of Applied Engineering Research . 2017,第22aPta8期

机译：扰流板角度对掀背模型空气动力学性能的影响
3. Influence of rear-roof spoiler on the aerodynamic performance of hatchback vehicle [J] . MATEC Web of Conferences . 2017,第1期

机译：后扰流板对掀背车空气动力性能的影响
4. CFD study of aerodynamic sensitivity to air deviation angle for a hatchback vehicle [C] . L Ilea, D Iozsa, C Stan Innovative Manufacturing Engineering and Energy Conference . 2019

机译：斜拉车辆空气动力敏感性的CFD研究
5. Aerodynamic performance and particle image velocimetery of piezo actuated biomimetic manduca sexta engineered wings towards the design and application of a flapping wing flight vehicle. [D] . DeLuca, Anthony M. 2013

机译：压电致动仿生曼陀罗六边形工程机翼的气动性能和颗粒图像速度计，用于扑翼飞行器的设计和应用。
6. Aerodynamic Performance of a Passive Pitching Model on Bionic Flapping Wing Micro Air Vehicles [O] . Jinjing Hao, Jianghao Wu, Yanlai Zhang 2019

机译：仿生拍打翼微型飞机被动俯仰模型的空气动力学性能
7. Aerodynamic performance of several passive vortex generator configurations on an Ahmed body subjected to yaw angles [O] . H. Viswanathan 2021

机译：几种被动涡流发生器配置的空气动力学性能对偏航角度的艾哈迈德机身上的配置
8. Powered Model Investigation of the Effects of Gated Spoilers on the Aerodynamic Characteristics of Wings at Angles of Attack from 0 to 90 Degrees [R] . Reader, K. R., Murphy, R. D. 1967

机译：控制扰流板对0~90度攻角下翼翼气动特性影响的动力模型研究

Yaw angle effect on the aerodynamic performance of hatchback vehicle fitted with wing spoiler

著录项

引文网络

相似文献

相关主题

期刊订阅