Improved understanding of transonic flutter: A three-parameter flutter surface
Publication
, Journal Article
Kholodar Denis, B; Dowell Earl, H; Thomas Jeffrey, P; Hall Kenneth, C
Published in: Journal of Aircraft
2004
An understanding of transonic flutter is often critical for high-speed aircraft development. A presentation of the transonic flutter velocity as a function of the Mach number and mass ratio is shown here to provide many advantages. Such a presentation offers new insights when comparing computational and wind-tunnel flutter results. The benefits of such a presentation are also evident in parameter studies. Finally, the subject of flutter similarity rules for airfoils of different thicknesses is also addressed.
Duke Scholars
Published In
Journal of Aircraft
Publication Date
2004
Volume
41
Issue
4
Start / End Page
911 / 917
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). Improved understanding of transonic flutter: A three-parameter flutter surface. Journal of Aircraft, 41(4), 911–917.
Kholodar Denis, B., H. Dowell Earl, P. Thomas Jeffrey, and C. Hall Kenneth. “Improved understanding of transonic flutter: A three-parameter flutter surface.” Journal of Aircraft 41, no. 4 (2004): 911–17.
Kholodar Denis B, Dowell Earl H, Thomas Jeffrey P, Hall Kenneth C. Improved understanding of transonic flutter: A three-parameter flutter surface. Journal of Aircraft. 2004;41(4):911–7.
Kholodar Denis, B., et al. “Improved understanding of transonic flutter: A three-parameter flutter surface.” Journal of Aircraft, vol. 41, no. 4, 2004, pp. 911–17.
Kholodar Denis B, Dowell Earl H, Thomas Jeffrey P, Hall Kenneth C. Improved understanding of transonic flutter: A three-parameter flutter surface. Journal of Aircraft. 2004;41(4):911–917.
Published In
Journal of Aircraft
Publication Date
2004
Volume
41
Issue
4
Start / End Page
911 / 917
Related Subject Headings
- Aerospace & Aeronautics
- 40 Engineering
- 09 Engineering