Supersonic flutter analysis based on a local piston theory

AIAA Journal

Volumn 47, Issue 10, 2009, Pages 2321-2328

  Zhang, Wei Wei ^a,c   Ye, Zheng Yin ^a,c   Zhang, Chen An ^a,c   Liu, Feng ^b,d  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

^b UNIVERSITY OF CALIFORNIA   (United States)

^c National Key Laboratory of Aerodynamic Design and Research   (China)

^d Department of Mechanical and Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIR LOADS; AIRFOIL SURFACES; BLUNT LEADING EDGES; COMPUTATIONAL TIME; EULER METHOD; LOCAL MEAN; LOCAL PISTON THEORY; MEAN FLOW; PISTON THEORY; SUPERSONIC AND HYPERSONIC; SUPERSONIC FLUTTER; UNSTEADY PRESSURES;

ANGLE OF ATTACK INDICATORS; FLUTTER (AERODYNAMICS); MACH NUMBER;

AIRFOILS;

EID: 72549108577     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.37750     Document Type: Article

References (15)

1. Gupta, K. K., and Voelker, L. S., "CFD-Based Aeroelastic Analysis of the X-43 Hypersonic Flight Vehicle," AIAA Paper 01-0712, 2001.
2. Alonso, J. J., and Jameson, A., "Fully-Implicit Time-Marching Aeroelastic Solutions," AIAA Paper 94-10056, 1994.
3. Liu, F., Cai, J., Zhu, Y., Tsai, H. M., andWong, A. S. F., "Calculation of Wing Flutter by a Coupled Fluid-Structure Method," Journal of Aircraft, Vol.38, No.2, 2001, pp. 334-342. doi:10.2514/2.2766
4. Friedmann, P., McNamara, J. J., Thuruthimattam, B. J., and Nydick, I., "Aeroelastic Analysis of Hypersonic Vehicles," Journal of Fluids and Structures, Vol.19, No.5, 2004, pp. 681-712. doi:10.1016/j.jfluidstructs.2004. 04.003 (Pubitemid 38825759)
5. Lighthill, M. J., "Oscillating Airfoils at High Mach Number," Journal of the Aeronautical Sciences, Vol.20, No.6, 1953, pp. 402-406.
6. Van Dyke, M. D., "Supersonic Flow Past Airfoils Including Nonlinear Thickness Effect," NACA 1183, 1953.
7. Ashley, H., and Zartarian, G., "Piston Theory-A New Aerodynamic Tool for the Aeroelastician," Journal of the Aeronautical Sciences, Vol.23, No.12, 1956, pp. 1109-1118.
8. Mei, C., Abdel-Motagaly, K., and Chen, R. R., "Review of Nonlinear Panel Flutter at Supersonic and Hypersonic speeds," Applied Mechanics Reviews, Vol.52, No.10, 1999, pp. 321-332. doi:10.1115/1.3098919
9. Liu, D. D., Yao, Z. X., Sarhaddi, D., and Chaves, F., "From Piston Theory to a Unified Hypersonic Supersonic Lifting Surface Method," Journal of Aircraft, Vol.34, No.3, 1997, pp. 304-312. doi:10.2514/2.2199
10. Liu, D. D., James, D. K., Chen, P. C., and Pototzky, A. S., "Further Studies of Harmonic Gradient Method for Supersonic Aeroelastic Applications," Journal of Aircraft, Vol.28, No.9, 1991, pp. 598-605. doi:10.2514/3.46070
11. Wang, G., "New Type of Grid Generation Technique together with the High Efficiency and High Accuracy Scheme Researches for Complex Flow Simulation," Ph.D. Dissertation, Northwestern Polytechnical Univ., Xi'an, China, 2005.
12. Zhang, W., "Efficient Analysis for Aeroelasticity Based on Computational Fluid Dynamics," Ph.D. Dissertation, Northwestern Polytechnical Univ., Xi'an, China, 2006 (in Chinese).
13. Zhang, W., and Ye, Z., "Two Better Loosely Coupled Solution Algorithms of CFD Based Aeroelastic Simulation," Engineering Applications of Computational Fluid Mechanics, Vol.1, No.4, 2007, pp. 253-262.
14. Zhang,W., and Ye, Z., "Control Law Design for Transonic Aeroservoelasticity," Aerospace Science and Technology,Vol. 11, Nos. 2-3, 2007, pp. 136-145. doi:10.1016/j.ast.2006.12.004 (Pubitemid 46483162)
15. Bai, K., Feng, M., and Fu, G., "Flutter Experiment for Supersonic Rudder," The Seventh Chinese Conference on Aeroelasticity, Huzhou, Zhejiang, China, Oct. 2001, pp. 40-46 (in Chinese).