Numerical Study of an Airfoil/Rotating-Slotted-Cylinder Based Flutter Exciter-Reference-Cited by-同舟云学术

Numerical Study of an Airfoil/Rotating-Slotted-Cylinder Based Flutter Exciter

Published:2015-11 Issue:6 Volume:52 Page:2100-2105
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Xu Heyong¹,Xing Shilong¹,Ye Zhengyin¹

Affiliation:

1. National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033327

Reference15 articles.

1. KehoeM. W. “Flutter and Aeroservoelastic Clearance of the X-29A Forward-Swept Wing Airplane,” NASA TM-100447, Sept. 1989.

2. LaureP.MilletM.PiazzoliG. “Pyrotechnic Bonkers for Structural Tests in Flight,” ONERA TP-1389E 1974.

3. VernonL. “In-Flight Investigation of a Rotating Cylinder-Based Structural Excitation System for Flutter Testing,” NASA TM-4512, June 1993.

4. WeissF.SchweigerJ.HonlingerH. “Flutter Flight Test of the RANGER 2000 Aircraft,” AGARD CP-566, Nov. 1995.

5. SchippersP.PersoonA. J. “Flight Flutter Testing of a Turbo-Prop Aircraft by Using External Excitation Devices,” AGARD CP-566, Nov. 1995.

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