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Limit-cycle oscillations of a typical airfoil in transonic flow

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

Using an inviscid flow computational-fluid-dynamic model and a harmonic balance flow solver, a parametric investigation of how structural-inertial parameters and freestream Mach number of a transonic flow affect the limit-cycle oscillation characteristics of a typical two-degree-of-freedom transonic airfoil configuration is presented. The computational efficiency of the harmonic balance aerodynamic model allows a much more thorough exploration of the parameter range than has been possible previously.

Duke Scholars

Published In

Journal of Aircraft

Publication Date

2004

Volume

41

Issue

5

Start / End Page

1067 / 1072

Related Subject Headings

  • Aerospace & Aeronautics
  • 40 Engineering
  • 09 Engineering
 

Citation

APA
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ICMJE
MLA
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Kholodar Denis, B., Dowell Earl, H., Thomas Jeffrey, P., & Hall Kenneth, C. (2004). Limit-cycle oscillations of a typical airfoil in transonic flow. Journal of Aircraft, 41(5), 1067–1072.
Kholodar Denis, B., H. Dowell Earl, P. Thomas Jeffrey, and C. Hall Kenneth. “Limit-cycle oscillations of a typical airfoil in transonic flow.” Journal of Aircraft 41, no. 5 (2004): 1067–72.
Kholodar Denis B, Dowell Earl H, Thomas Jeffrey P, Hall Kenneth C. Limit-cycle oscillations of a typical airfoil in transonic flow. Journal of Aircraft. 2004;41(5):1067–72.
Kholodar Denis, B., et al. “Limit-cycle oscillations of a typical airfoil in transonic flow.” Journal of Aircraft, vol. 41, no. 5, 2004, pp. 1067–72.
Kholodar Denis B, Dowell Earl H, Thomas Jeffrey P, Hall Kenneth C. Limit-cycle oscillations of a typical airfoil in transonic flow. Journal of Aircraft. 2004;41(5):1067–1072.

Published In

Journal of Aircraft

Publication Date

2004

Volume

41

Issue

5

Start / End Page

1067 / 1072

Related Subject Headings

  • Aerospace & Aeronautics
  • 40 Engineering
  • 09 Engineering