@inproceedings{oai:jaxa.repo.nii.ac.jp:00005656,
 author = {Ly, Eddie and 中道, 二郎 and Ly, Eddie and Nakamichi, Jiro},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling},
 month = {Feb},
 note = {The effect of small perturbations on steady nonlinear transonic small disturbance flow-fields, in the context of two-dimensional flows governed by the general-frequency transonic small disturbance equation with nonreflecting far-field boundary conditions, is investigated. This paper presents a time-linearized time-domain solution method that includes effects due to the shock-generated entropy and vorticity and shock wave motions. The solution procedure correctly accounts for the small-amplitude shock wave motion due to small unsteady changes in the aerofoil boundary conditions, and correctly models a flow-field with embedded strong shock waves. Steady and first harmonic pressure distributions for the NACA 0003 aerofoil with a harmonically oscillating flap, and NACA 0012 aerofoil undergoing a sinusoidal pitching oscillation, are predicted and compared with the Euler results., 資料番号: AA0063824001, レポート番号: JAXA-SP-07-008E},
 pages = {1--8},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Efficient time-linearized TSD computations including the effects of shock-generated entropy, vorticity and shock wave motion},
 volume = {JAXA-SP-07-008E},
 year = {2008}
}