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Modeling viscous transonic limit-cycle oscillation behavior using a harmonic balance approach

Publication ,  Journal Article
Thomas Jeffrey, P; Dowell Earl, H; Hall Kenneth, C
Published in: Journal of Aircraft
2004

Presented is a harmonic-balance computational fluid dynamic approach for modeling limit-cycle oscillation behavior of aeroelastic airfoil configurations in a viscous transonic flow. For the NLR 7301 airfoil configuration studied, accounting for viscous effects is shown to significantly influence computed limit-cycle oscillation trends when compared to an inviscid analysis. A methodology for accounting for changes in mean angle of attack during limit-cycle oscillation is also developed.

Duke Scholars

Published In

Journal of Aircraft

Publication Date

2004

Volume

41

Issue

6

Start / End Page

1266 / 1274

Related Subject Headings

  • Aerospace & Aeronautics
  • 40 Engineering
  • 09 Engineering
 

Citation

APA
Chicago
ICMJE
MLA
NLM
Thomas Jeffrey, P., Dowell Earl, H., & Hall Kenneth, C. (2004). Modeling viscous transonic limit-cycle oscillation behavior using a harmonic balance approach. Journal of Aircraft, 41(6), 1266–1274.
Thomas Jeffrey, P., H. Dowell Earl, and C. Hall Kenneth. “Modeling viscous transonic limit-cycle oscillation behavior using a harmonic balance approach.” Journal of Aircraft 41, no. 6 (2004): 1266–74.
Thomas Jeffrey P, Dowell Earl H, Hall Kenneth C. Modeling viscous transonic limit-cycle oscillation behavior using a harmonic balance approach. Journal of Aircraft. 2004;41(6):1266–74.
Thomas Jeffrey, P., et al. “Modeling viscous transonic limit-cycle oscillation behavior using a harmonic balance approach.” Journal of Aircraft, vol. 41, no. 6, 2004, pp. 1266–74.
Thomas Jeffrey P, Dowell Earl H, Hall Kenneth C. Modeling viscous transonic limit-cycle oscillation behavior using a harmonic balance approach. Journal of Aircraft. 2004;41(6):1266–1274.

Published In

Journal of Aircraft

Publication Date

2004

Volume

41

Issue

6

Start / End Page

1266 / 1274

Related Subject Headings

  • Aerospace & Aeronautics
  • 40 Engineering
  • 09 Engineering