Hostname: page-component-76fb5796d-5g6vh Total loading time: 0 Render date: 2024-04-26T10:36:16.768Z Has data issue: false hasContentIssue false
  • English
  • Français

Stability criteria of Samara-like decelerator in unsteady transitions

Published online by Cambridge University Press:  02 December 2022

H.-C. Wang Open the ORCID record for H.-C. Wang [Opens in a new window]  and
R.E. Breidenthal Open the ORCID record for R.E. Breidenthal [Opens in a new window]
H.-C. Wang*
Affiliation:
ZeroAvia, Inc., Engineering of Aircraft Integration, Hollister, CA, USA
R.E. Breidenthal
Affiliation:
University of Washington, Department of Aeronautics & Astronautics, Seattle, WA, USA
*
*Corresponding author. Email: hungchiwang1993@gmail.com
Get access Rights & Permissions [Opens in a new window]

Abstract

The physics behind the transitions of natural Samaras, or the bio-inspired counterparts, to steady autorotation has been unclear. Theoretical and experimental investigations explore the inertial and aerodynamic characteristics required to guarantee stable transitions of an artificial Samara-like decelerator from chaotic tumbling motions to azimuthal autorotation. A non-dimensional inertial criterion is proposed, which is in accord with experiments.

Keywords

SamaraAutorotationDeceleratorStabilityFlight dynamicsFlying quality
Type
Research Article
Information
The Aeronautical Journal , Volume 127 , Issue 1312 , June 2023 , pp. 879 - 899
Check for updates
Copyright
© The Author(s), 2022. Published by Cambridge University Press on behalf of Royal Aeronautical Society

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Norberg, R. Autorotation, self-stability, and structure of single-winged fruits and seeds (Samaras) with comparative remarks on animal flight, Biolog. Rev., 1973, 48, pp 561–596.Google Scholar
Kellas, A. The guided Samara: Design and development of a controllable single-bladed autorotating vehicle, 2007.Google Scholar
Varshney, K., Chang, S. and Wang, Z.J. The kinematics of falling maple seeds and the initial transition to a Helical motion, Nonlinearity, December 2012, 25, pp C1.CrossRefGoogle Scholar
Azuma, A. and Yasuda, K. Flight performance of rotary seeds, J. Theor. Biol., 1989, 138, pp 23–53.CrossRefGoogle Scholar
Zhang, W., Mueller, M.W. and D’Andrea, R. A controllable flying vehicle with a single moving part, IEEE International Conference on Robotics and Automation (ICRA), 2016, pp 3275–3281.CrossRefGoogle Scholar
Lentink, D., Dickson, W.B., Van Leeuwen, J.L. and Dickinson, M.H. Leading-edge vortices elevate lift of autorotating plant seeds, Science (American Association for the Advancement of Science), 2009, 324, pp 1438–1440.CrossRefGoogle ScholarPubMed
Gessow, A. and Myers, G.C. Aerodynamics of the Helicopter, F. Ungar Pub., New York, 1967, pp 119–122.Google Scholar
Green, D.S. The terminal velocity and dispersal of spinning Samaras, Amer. J. Botany, 1980, 67, pp 1218–1224.CrossRefGoogle Scholar
Wick, B.H. Study of the subsonic forces and moments on an inclined plate of infinite span, NACA TN 3221, 1954.Google Scholar
Zipfel, P.H. Modeling and Simulation of Aerospace Vehicle Dynamics, American Institute of Aeronautics and Astronautics, Reston, 2000.Google Scholar
Schaub, H. and Junkins, J.L. Analytical Mechanics of Space Systems. Education Series, American Institute of Aeronautics and Astronautics, Reston, 2003.CrossRefGoogle Scholar