Parametric study of flutter for an airfoil in inviscid transonic flow
Publication
, Journal Article
Kholodar Denis, B; Thomas Jeffrey, P; Dowell Earl, H; Hall Kenneth, C
Published in: Journal of Aircraft
2003
A parametric study of flutter was conducted for an airfoil in inviscid transonic flow. An inviscid computational flow dynamic harmonic balance aerodynamic-Euler-based code was used for the investigation. The computational efficiency of the time-linearized option of the harmonic balance aerodynamic model allows a much more thorough exploration of the parameter range than was previously achieved.
Duke Scholars
Published In
Journal of Aircraft
Publication Date
2003
Volume
40
Issue
2
Start / End Page
303 / 313
Related Subject Headings
- Aerospace & Aeronautics
- 40 Engineering
- 09 Engineering
Citation
APA
Chicago
ICMJE
MLA
NLM
Kholodar Denis, B., Thomas Jeffrey, P., Dowell Earl, H., & Hall Kenneth, C. (2003). Parametric study of flutter for an airfoil in inviscid transonic flow. Journal of Aircraft, 40(2), 303–313.
Kholodar Denis, B., P. Thomas Jeffrey, H. Dowell Earl, and C. Hall Kenneth. “Parametric study of flutter for an airfoil in inviscid transonic flow.” Journal of Aircraft 40, no. 2 (2003): 303–13.
Kholodar Denis B, Thomas Jeffrey P, Dowell Earl H, Hall Kenneth C. Parametric study of flutter for an airfoil in inviscid transonic flow. Journal of Aircraft. 2003;40(2):303–13.
Kholodar Denis, B., et al. “Parametric study of flutter for an airfoil in inviscid transonic flow.” Journal of Aircraft, vol. 40, no. 2, 2003, pp. 303–13.
Kholodar Denis B, Thomas Jeffrey P, Dowell Earl H, Hall Kenneth C. Parametric study of flutter for an airfoil in inviscid transonic flow. Journal of Aircraft. 2003;40(2):303–313.
Published In
Journal of Aircraft
Publication Date
2003
Volume
40
Issue
2
Start / End Page
303 / 313
Related Subject Headings
- Aerospace & Aeronautics
- 40 Engineering
- 09 Engineering