AERODYNAMIC STUDY OF SLOTTED FLAP FOR NACA 24012 AIRFOIL BY DYNAMIC MESH TECHNIQUES AND VISUALIZATION FLOW-Reference-Cited by-同舟云学术

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AERODYNAMIC STUDY OF SLOTTED FLAP FOR NACA 24012 AIRFOIL BY DYNAMIC MESH TECHNIQUES AND VISUALIZATION FLOW

Published:2021-01-31 Issue: Volume: Page:230-239
ISSN:2148-7847
Container-title:Journal of Thermal Engineering
language:
Short-container-title:

Author:

HUSSEİN Emad,AZZİZ Haider,RASHİD Farhan

Publisher

Journal of Thermal Engineering

Subject

Fluid Flow and Transfer Processes,Energy Engineering and Power Technology,Building and Construction

Cited by 7 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. The Effect of Riblets on the Aerodynamic Performance of NACA 0018 Airfoil;Çukurova Üniversitesi Mühendislik Fakültesi Dergisi;2024-03-28

2. Design of a Novel Aerofoil of a Light Aircraft for Robust Aerodynamic Performance at High Reynolds Number Regime Using XFLR5;Arabian Journal for Science and Engineering;2024-02-26

3. NumericalStudy of Turbulent Flows over a NACA 0012 Airfoil: Insights into Its Performance and the Addition of a Slotted Flap;Applied Sciences;2023-07-05

4. Experimental Study of Fluid Flow Characteristics in Wing Airfoil Naca 43018 with Parabolic Vortex Generator Using Oil Flow Visualization;Proceedings of the International Conference on Advance Transportation, Engineering, and Applied Science (ICATEAS 2022);2023

5. Numerical Simulation of Effect Modification of Single Slotted Flap on Wing Cessna C208B Grand Caravan for Aerodynamic Performance;Proceedings of the International Conference on Advance Transportation, Engineering, and Applied Science (ICATEAS 2022);2023

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