Numerical study of a supercritical airfoil/wing with variable-camber technology-Reference-Cited by-同舟云学术

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Numerical study of a supercritical airfoil/wing with variable-camber technology

Published:2020-07 Issue:7 Volume:33 Page:1850-1866
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

NIU Wei,ZHANG Yufei,CHEN Haixin,ZHANG Miao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference33 articles.

1. Advanced tube and wing aircraft for year 2050 timeframe;Heinemann,2017

2. Aerodynamic design of transport aircraft;Obert,2009

3. The next decade in commercial aircraft aerodynamics – A Boeing perspective;Goldhammer,2011

4. Optimized off-design performance of flexible wings with continuous trailing-edge flaps;Rodriguez,2015

5. Global aerodynamic design optimization based on data dimensionality reduction;Qiu;Chin J Aeronaut,2018

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1. Optimizing the Aerodynamic Efficiency of Different Airfoils by Altering Their Geometry at Low Reynolds Numbers;Arabian Journal for Science and Engineering;2024-04-16

2. Hovering performance analysis of helicopter rotor blades using supercritical airfoil;Aircraft Engineering and Aerospace Technology;2024-01-25

3. Numerical and experimental studies of a morphing airfoil with trailing edge high-frequency flapping;Physics of Fluids;2023-12-01

4. Electroactive morphing effects on the aerodynamic performance through wobulation around an A320 wing with vibrating trailing edge at high Reynolds number;Journal of Fluids and Structures;2023-11

5. Design and Optimization of a Hinged Mechanism Guiding Flap to Three Positions;Journal of Aircraft;2023-05

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