Analysis and Computational Study of the Aerodynamics, Aeroelasticity and Flight Dynamics of Flapping-Wing Ornithopter Using Linear Approximation-Reference-Cited by-同舟云学术

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Analysis and Computational Study of the Aerodynamics, Aeroelasticity and Flight Dynamics of Flapping-Wing Ornithopter Using Linear Approximation

Published:2023 Issue: Volume: Page:863-893
ISSN:
Container-title:Introduction to Aeroelasticity
language:
Short-container-title:

Author:

Djojodihardjo Harijono

Publisher

Springer Nature Singapore

Link

https://link.springer.com/content/pdf/10.1007/978-981-16-8078-6_23

Reference30 articles.

1. Anderson, M.L. 2011. Design and Control of Flapping Wing Micro Air Vehicles. Ph.D. Thesis, AFIT, dayton, USA.

3. Chikamurti, S.K. 2009. A Computational Aeroelasticity Framework for Analyzing Flapping Wings. Ph.D. Thesis, University of Michigan.

4. Dai, H., F.-B. Tian, J. Song, and H. Luo. 2012. Aerodynamics and Aeroelasticity of Flapping Wings. Nashville, Tennessee, USA: Department of Mechanical Engineering, Vanderbilt University, ICTAM.

5. DeLaurier, J.D. 1993. An aerodynamic model for flapping wing flight. Aeronautical Journal of the Royal Aeronautical Society 97: 125–130.

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