Supersonic Flutter Analysis Based on a Local Piston Theory

@inproceedings{Zhang2009SupersonicFA,
  title={Supersonic Flutter Analysis Based on a Local Piston Theory},
  author={Wei-Wei Zhang and Zheng-Yin Ye and Chunxin Zhang and Feng Liu},
  year={2009}
}
A highly efficient local-piston theory is presented for the prediction of inviscid unsteady pressure loads at supersonic and hypersonic speeds. A steady mean flow solution is first obtained by an Euler method. The classical piston theory ismodified to apply locally at each point on the airfoil surface on top of the localmean flow to obtain the unsteadypressureperturbations causedby thedeviation of the airfoil surface from itsmean locationwithout the need of performing unsteady Euler… CONTINUE READING
Highly Cited
This paper has 29 citations. REVIEW CITATIONS

Citations

Publications citing this paper.
Showing 1-8 of 8 extracted citations

Adaptive output feedback control of flow-induced vibrations of a membrane at high mach numbers

2017 IEEE 56th Annual Conference on Decision and Control (CDC) • 2017
View 1 Excerpt

Aerodynamic optimization for hypersonic airfoil design based on local piston theory

2016 13th International Bhurban Conference on Applied Sciences and Technology (IBCAST) • 2016
View 1 Excerpt

References

Publications referenced by this paper.
Showing 1-10 of 16 references

Control Law Design for Transonic Aeroservoelasticity

W. Zhang, Z. Ye
Aerospace Science and Technology • 2007

Control Law Design for Transonic Aeroservoelasticity,”Aerospace

W. Zhang, Z. Ye
Science and Technology, Vol. 11,Nos • 2007

Two Better Loosely Coupled Solution Algorithms of CFD Based Aeroelastic Simulation,

W. Zhang, Z. Ye
Engineering Applications of Computational Fluid Mechanics, • 2007
View 1 Excerpt

Efficient Analysis for Aeroelasticity Based on Computational Fluid Dynamics,

W. Zhang
Ph.D. Dissertation, Northwestern Polytechnical Univ., Xi’an, China, • 2006
View 2 Excerpts

New Type of Grid Generation Technique together with the High Efficiency and High Accuracy Scheme Researches for Complex Flow Simulation,

G. Wang
2005
View 1 Excerpt

CFD-Based Aeroelastic Analysis of the X-43 Hypersonic Flight Vehicle,

K. K. Gupta, L. S. Voelker
AIAA Paper 01-0712, • 2001

Flutter Experiment for Supersonic Rudder,

K. Bai, M. Feng, G. Fu
The Seventh Chinese Conference on Aeroelasticity, • 2001
View 1 Excerpt

Review of Nonlinear Panel Flutter at Supersonic and Hypersonic speeds,

C. Mei, K. Abdel-Motagaly, R. R. Chen
Applied Mechanics Reviews, • 1999
View 1 Excerpt

From Piston Theory to a Unified Hypersonic Supersonic Lifting Surface Method,

D. D. Liu, Z. X. Yao, D. Sarhaddi, F. Chaves
Journal of Aircraft, • 1997
View 2 Excerpts