1. Stability derivatives for a delta-wing X-31 aircraft validated using wind tunnel test data;Anton;Proc. IMechE Part G: J. Aerspace Eng.,2010
2. S. Schmidt, D.M. Newman, Estimation of dynamic stability derivatives of a generic aircraft, in: Proceedings of the 17th Australian Fluid Mechanics Conference, Auckland, New Zealand, 2010, pp. 1–4.
3. K.J. Orlik-Rückeman, Review of Techniques for the Determination of Dynamic Stability Parameters in Wind Tunnels, AGARD-LS-114 The Advisory Group for Aerospace Research and Development, NATO Research and Technology Organization, Brussels, Belgium, 1981.
4. E.S. Hanff, Direct Forced-oscillation Techniques for the Determination of Stability Derivatives in Wind Tunnels, AGARD-LS-114 The Advisory Group for Aerospace Research and Development, NATO Research and Technology Organization, Brussels, Belgium, 1981.
5. Dynamic stability derivatives of a maneuvering combat aircraft model;Altun;J. Aeronaut. Space Technol.,2004