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Computational evaluation of the performance of lifting surfaces with leading-edge protuberances

Publication ,  Journal Article
Weber, PW; Howle, LE; Murray, MM; Miklosovic, DS
Published in: Journal of Aircraft
January 1, 2011

The leading-edge tubercles of humpback whale flippers have been shown to enhance hydrodynamic performance by increasing lift and decreasing drag poststall. To explore this effect, computational simulations of two models based on an idealized humpback whale flipper were conducted, one with a smooth leading edge and one with simulatedleading-edge tubercles. Two different commercial computational fluid dynamics packages were used, STAR-CCM+ and SolidWorks Flow Simulation, and the results were compared with experiment. Numeric lift predictions in the nonstall region were reasonably accurate (maximum error 6.6% between both codes), while lift predictions in the poststall region were problematic. Numeric drag predictions in the early nonstall region were within experimental error for STAR-CCM+ using the Spalart-Allmaras turbulence model, while both codes exhibited drag prediction error in the stall region. Flow visualizations showed that the smooth flipper exhibited trailing-edge stall, while the simulated tubercle flipper stalled in the troughs, behind the leading notches, first. At high angles of attack, the simulated tubercle flipper still possessed significant regions of attached flow, which contributes to its ability to maintain increased lift poststall. © Copyright 2010.

Duke Scholars

Published In

Journal of Aircraft

DOI

EISSN

1533-3868

ISSN

0021-8669

Publication Date

January 1, 2011

Volume

48

Issue

2

Start / End Page

591 / 600

Related Subject Headings

  • Aerospace & Aeronautics
  • 40 Engineering
  • 09 Engineering
 

Citation

APA
Chicago
ICMJE
MLA
NLM
Weber, P. W., Howle, L. E., Murray, M. M., & Miklosovic, D. S. (2011). Computational evaluation of the performance of lifting surfaces with leading-edge protuberances. Journal of Aircraft, 48(2), 591–600. https://doi.org/10.2514/1.C031163
Weber, P. W., L. E. Howle, M. M. Murray, and D. S. Miklosovic. “Computational evaluation of the performance of lifting surfaces with leading-edge protuberances.” Journal of Aircraft 48, no. 2 (January 1, 2011): 591–600. https://doi.org/10.2514/1.C031163.
Weber PW, Howle LE, Murray MM, Miklosovic DS. Computational evaluation of the performance of lifting surfaces with leading-edge protuberances. Journal of Aircraft. 2011 Jan 1;48(2):591–600.
Weber, P. W., et al. “Computational evaluation of the performance of lifting surfaces with leading-edge protuberances.” Journal of Aircraft, vol. 48, no. 2, Jan. 2011, pp. 591–600. Scopus, doi:10.2514/1.C031163.
Weber PW, Howle LE, Murray MM, Miklosovic DS. Computational evaluation of the performance of lifting surfaces with leading-edge protuberances. Journal of Aircraft. 2011 Jan 1;48(2):591–600.

Published In

Journal of Aircraft

DOI

EISSN

1533-3868

ISSN

0021-8669

Publication Date

January 1, 2011

Volume

48

Issue

2

Start / End Page

591 / 600

Related Subject Headings

  • Aerospace & Aeronautics
  • 40 Engineering
  • 09 Engineering