Modern Wind Tunnel Techniques for Unsteady Testing – Development of Dynamic Test Rigs

Author:

Bergmann A.

Publisher

Springer Berlin Heidelberg

Reference31 articles.

1. Orlik-Rückemann, K.: Methods of Measurement of Aircraft Dynamic Stability Derivatives, National Research Laboratories NRC, Canada, LR-254 (1959)

2. Orlik-Rückemann, K.: Review of Techniques for Determination of Dynamic Stability Parameters in Wind Tunnels., AGARD-LS-114, pp. 3-1–3-28 (1981)

3. Bergmann, A., et al.: Experimental and Numerical Research on the Aerodynamics of Unsteady Moving Aircraft. In: Progress in Aerospace Sciences, vol. 44. Elsevier, Amsterdam (in press, 2008)

4. Loeser, T.: Experimental Research of Dynamic Derivatives of Unsteady Moved Aircraft. In: VKI Lecture Series on Experimental Determination of Dynamic Stability Parameters (2008)

5. Loeser, T., Bergmann, A.: Development of the Dynamic Wind Tunnel Capabilities at DNW-NWB. In: Proceedings of the 41st AIAA Meeting, AIAA 2003-0453, Reno (2003)

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