Aerodynamics of Flapping and Plunging Wings using Particle Image Velocimetry Measurements
Abstract
Understanding the aerodynamic characteristics of flapping and plunging wings at low Reynolds numbers is necessary for advancing Micro Air Vehicle research and development. The flow fields around a variety of wings were investigated with Particle Image Velocimetry and hydrogen bubble flow visualization. The effects of reduced frequency, angle of attack, and wing size and shape were analyzed using the acquired data. Vortex shedding begins earlier at higher angles of attack and at lower reduced frequencies. The wing produces thrust via a jet wake.
Recommended Citation
T. A. Swanson and K. M. Isaac, "Aerodynamics of Flapping and Plunging Wings using Particle Image Velocimetry Measurements," Proceedings of the 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition (2009, Orlando, FL), American Institute of Aeronautics and Astronautics (AIAA), Jan 2009.
Meeting Name
47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition (2009: Jan. 5-8, Orlando, FL)
Department(s)
Mechanical and Aerospace Engineering
Keywords and Phrases
Aerodynamic Characteristics; Flapping Wings; Plunging Wings
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2009 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
Publication Date
08 Jan 2009
