Pressure Distribution on an Airfoil in Nonuniform Motion

Author:

Neumark S.1

Affiliation:

1. Royal Aircraft Establishment, Farnborough, Hants., England

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Reference5 articles.

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. Deep reinforcement learning of airfoil pitch control in a highly disturbed environment using partial observations;Physical Review Fluids;2024-09-12

2. On Aerodynamic Models for Flutter Analysis: A Systematic Overview and Comparative Assessment;Applied Mechanics;2021-07-29

3. Unsteady thin airfoil theory revisited for a general deforming airfoil;Journal of Mechanical Science and Technology;2010-12

4. Actuator-Work Concepts Applied to Unconventional Aerodynamic Control Devices;10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2004-08-30

5. On aerodynamic modelling of an insect–like flapping wing in hover for micro air vehicles;Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences;2002-01-11

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