Numerical Simulation of T-Tail Flutter in Subsonic and Transonic Flows
Author:
Affiliation:
1. Professor Emeritus, Kyushu University
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/tjsass/67/5/67_T-23-42/_pdf
Reference18 articles.
1. 1) Baldock, J. C. A.: The Determination of the Flutter Speed of a T-Tail Unit by Calculations, Model Tests and Flight Flutter Tests, AGARD Report 221, 1958.
2. 2) Washizu, K., Ichikawa, T., and Adachi, T.: A Note on T-Tail Flutter, J. Jpn. Soc. Aeronaut. Space Sci., 18 (1970), pp. 327–333 (in Japanese).
3. 3) Jennings, W. P. and Berry, M. A.: Effect of Stabilizer Dihedral and Static Lift on T-Tail Flutter, J. Aircraft, 14 (1977), pp. 364–367.
4. 4) Van Zyl, L. W. and Mathews, E. H.: Aeroelastic Analysis of T-Tails Using an Enhanced Doublet Lattice Method, J. Aircraft, 48 (2011), pp. 823–831.
5. 5) Queijo, M. J.: Theory for Computing Span Loads and Stability Derivatives due to Sideslip, Yawing, and Rolling for Wings in Subsonic Compressible Flow, NASA TN D-4929, 1968.
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