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
Chicago
ICMJE
MLA
NLM
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