Design Optimization of Low Reynolds Number Airfoil for Enhanced Aerodynamics of 4R-UAV-Reference-Cited by-同舟云学术

Design Optimization of Low Reynolds Number Airfoil for Enhanced Aerodynamics of 4R-UAV

Published:2022-07-20 Issue: Volume: Page:
ISSN:
Container-title:2022 13th International Conference on Mechanical and Aerospace Engineering (ICMAE)
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Author:

Arshad Ali¹,Nawanjana Chameera¹,Kovalcuks Vadims¹

Affiliation:

1. Riga Technical University,Institute of Aeronautics, Faculty of Mechanical Engineering, Transport, and Aeronautics,Riga,Latvia

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9852822/9852497/09852511.pdf?arnumber=9852511

Reference15 articles.

1. A simplified design approach for high-speed wind tunnels. Part II: Diffuser optimization and complete duct design;arshad;Journal of Mechanical Science and Technology,2020

2. Computational Study of Noise Reduction in CFM56-5B Using Core Nozzle Chevrons

3. Stability Analysis for a Concept Design of Vertical Take-off and Landing (VTOL) Unmanned Aerial Vehicle (UAV)

4. Design optimization for the weight reduction of 2-cylinder reciprocating compressor crankshaft;arshad;Journal Archives of Mechanical Engineerig,2021

5. Summary of low-speed airfoil data;broeren,1995

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