Treatment of forced flap motions for aeroelastic simulations of an arrow wing

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 2, Issue , 2005, Pages 719-734

  Rampurawala, Abdul M ^a,b   Badcock, Ken J ^a,c  

^a UNIVERSITY OF GLASGOW   (United Kingdom)

^b CFD Laboratory   (United Kingdom)

^c Dept of Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FINITE ELEMENT METHOD; OSCILLATIONS; PRESSURE DISTRIBUTION;

FORCED FLAP MOTIONS; FORCED FLAP OSCILLATIONS; SURFACE OSCILLATION;

AERODYNAMICS;

EID: 28844451632     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-4962     Document Type: Conference Paper

References (17)

1. Schuster, D. M., Liu, D. D., and Huttsell, L. J., "Computational Aeroelasticity: Success, Progress, Challenge," Journal of Aircraft, Vol. 40, No. 5, 2003, pp. 843-856.
2. Bharadwaj, B. K., "Computation of Steady and Unsteady Control Surface Loads in Transonic Flow," AIAA paper 90-0935, 1990.
3. Obayashi, S. and Guruswamy, G., "Navier-Stokes Computations for Oscillating Control Surfaces," AIAA paper 92-4431, 1992.
4. Obayashi, S., Chiu, I. T., and Guruswamy, G., "Navier-Stokes Computations on Full Span Wing Body Configuration for Oscillating Control Surfaces," AIAA paper 93-3687, 1993.
5. Klopfer, G. H. and Obayashi, S., "Virtual Zone Navier-Stokes Computations for Oscillating Control Surfaces," AIAA paper 93-3363, 1993.
6. Karlsson, A. and Winzell, B., "Unsteady Control Surface Pressure Measurements and Computations," AIAA paper 96-2417, 1996.
7. Cole, H. S., Andrew, A. S., and Gupta, K., "Application of the Transpiration Method for Aeroservoelastic Prediction Using CFD," AIAA paper 98-2071, 1998.
8. Ide, H. and Ominsky, D., "Simulation of Static and Dynamic Aeroelastic Behavior of a Flexible Wing with Multiple Control Surface," AIAA paper 90-1075, April 1990.
9. Cole, H. S., Andrew, A. S., and Gupta, K., "CFD-Based Aeroservoelastic Predictions with Comparisons to Benchmark Experimental Data," AIAA paper 99-0766, Jan. 1999.
10. Yeh, D. T., "Aeroelastic Analysis of a Hinged-Flap and Control Surface Effectiveness Using the Navier-Stokes Equations," AIAA paper 95-02263, 1995.
11. Schuster, D. M. and Bartels, R. E., "Benchmark Active Control Technology (BACT) Wing CFD Results," Verification an Validation Data for Computational Unsteady Aerodynamics, RTO Technical Report - 26, October 2000, pp. 225-238.
12. M. Tamayama, K. Saitoh, H. M. and Nakamichi, J., "NAL SST Arrow Wing with Oscillating Flap," Verification an Validation Data for Computational Unsteady Aerodynamics, RTO Technical Report-26, October 2000, pp. 295-318.
13. Tamayama, M. and Nakamichi, J., "Unsteady Aerodynamics Measurements on an Elastic Wing Model of SST," AIAA paper 97-0836, Jan. 1997.
14. Badcock, K. J., Woodgate, M. A., and Richards, B. E., "Elements of Computational Fluid Dynamics on Block Structured Grids using Implicit Solvers," Progress in Aerospace Sciences, Vol. 36, 2000, pp. 351-392.
15. Goura, G. S. L., Time marching analysis of flutter using Computational Fluid Dynamics, Ph.D. thesis, University of Glasgow, 2001.
16. Goura, G. S. L., Badcock, K. J., Woodgate, M. A., and Richards, B. E., "Implicit Method for the Time Marching Analysis of Flutter," Royal Aeronautical Journal, Vol. 105, 2001, pp. 199-214.
17. Gordon, W. J. and Hall, C. A., "Construction of Curvilinear Coordinate Systems amd Applications to Mesh Generation," International Journal of Numerical Methods in Engineering, Vol. 7, 1973, pp. 461-477.