Have a personal or library account? Click to login
Computational Determination of Dynamic Stability Derivatives Cover

Computational Determination of Dynamic Stability Derivatives

By: Janusz Sznajder  
Open Access
|Dec 2025

References

  1. Orlik-Rückemann KJ. Techniques for dynamic stability testing in wind tunnels. In: Fluid Dynamics Panel Symposium; 22–24 May 1978; Athens, Greece. AGARD Conference Proceedings No. 235; 1978.
  2. Coe PL, Newsom WA Jr. Wind-tunnel investigations to determine the low-speed yawing stability derivatives of a twin-jet fighter model at high angles of attack. NASA-TN 7721; 1974.
  3. Roskam J. Airplane Flight Dynamics and Automatic Flight Controls. Part 1. Lawrence (KS): DAR Corporation; 2001.
  4. Da Ronch A, et al. Evaluation of dynamic derivatives using computational fluid dynamics. AIAA J. 2012;50(2).
  5. Granata D, et al. Numerical evaluation of aircraft aerodynamic static and dynamic stability derivatives by a mid-fidelity approach. Aerospace. 2024.
  6. Ghoreyshi M, et al. Indicial methods for the numerical calculation of dynamic derivatives of a finned projectile. In: AIAA Aviation Forum; 13–17 June 2016; Washington (DC). 46th AIAA Fluid Dynamics Conference.
  7. Jenkins JE. Dynamic derivatives. Wright-Patterson Air Force Base (OH): Air Force Research Laboratory, Aerospace Systems Directorate; 2015. AFRL-RQ-WP-TR- 2015-0141.
  8. Oktay E, Akay HU. CFD predictions of dynamic derivatives for missiles. In: AIAA Conference; 2002. AIAA-2002-0276.
  9. Tobak M, Schiff LB. Aerodynamic mathematical modeling – Basic concepts. In: AGARD Dynamic Stability Parameters; 1981. Available from: https://archive.org/details/DTIC_ADA1037647
  10. ANSYS, Inc. ANSYS Fluent Theory Guide. Release 2024 R1; 2024. 120 Janusz Sznajder
  11. Murman SM. A reduced-frequency approach for calculating dynamic derivatives. In: 43rd Aerospace Sciences Meeting; 10–13 Jan 2005; Reno (NV). AIAA-2005- 0840.
  12. Madder CA, Martins JRRA. Computation of aircraft stability derivatives using an automatic-differentiation adjoint approach. AIAA J. 2011;49(12).
  13. Uselton BL, Uselton JC. Test mechanism for measuring pitch-damping derivatives of missile configurations at high angles of attack. Arnold Engineering Development Center, Von Karman Gas Dynamics Facility; 1975.
  14. Dupuis AD, Hathaway W. Aeroballistic range tests of the Basic Finner reference projectile at supersonic velocities. Defence Research Establishment, Valcartier (Quebec): Centre de Recherches Pour la Défense; 1997. DREV-TM-9703.
  15. Murawski T. Szybowiec dwumiejscowy Bocian. Available from: www.tmdale.prv.pl; 2021.
  16. Samoloty Polskie. SZD-9 Bocian. Available from: http://www.samolotypolskie.pl/samoloty/2844/86/SZD-9-Bocian
Language: English
Page range: 98 - 121
Submitted on: Sep 17, 2025
|
Accepted on: Nov 20, 2025
|
Published on: Dec 24, 2025
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2025 Janusz Sznajder, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.