Aerodynamic Analysis on Double Wedge Airfoil at Different Mach Numbers with Varying Angle of Attacks Using Computational Fluid Dynamics-Reference-Cited by-同舟云学术

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Aerodynamic Analysis on Double Wedge Airfoil at Different Mach Numbers with Varying Angle of Attacks Using Computational Fluid Dynamics

Published:2019-07 Issue: Volume: Page:
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Container-title:2019 International Conference on Computer, Communication, Chemical, Materials and Electronic Engineering (IC4ME2)
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Author:

Kabir Asif,Hossain S.M. Mokarram,Hafiz Ahsan,Sayeed Abdullah As

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9030693/9036475/09036555.pdf?arnumber=9036555

Cited by 4 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. Numerical and experimental study of the impact on aerodynamic characteristics of the NACA0012 airfoil;Open Engineering;2024-01-01

2. Comparative study over double wedge and biconvex airfoils for laminar flow using CFD;Journal of Physics: Conference Series;2022-07-01

3. Analytical Study of Double Wedge Airfoil for Supersonic Applications and Shape Modification for Subsonic Applications;International Journal of Advanced Research in Science, Communication and Technology;2022-05-18

4. Comparison of the aerodynamic performance of NACA 4415 and KFm based stepped airfoils;Proceedings of the 13th International Conference on Mechanical Engineering (ICME2019);2021

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