Validation study of aerodynamic analysis tools for design optimization of helicopter rotors

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2007, Pages 537-571

  Choi, Seongim ^a,c   Alonso, Juan J ^a,c   Weide, Edwin V D ^a,c   Sitaraman, Jaina ^b,c  

^a STANFORD UNIVERSITY   (United States)

^b NATIONAL INSTITUTE OF AEROSPACE   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; FLOW FIELDS; HELICOPTER ROTORS; NAVIER STOKES EQUATIONS; OPTIMIZATION; REYNOLDS NUMBER;

AERODYNAMIC ANALYSIS TOOLS; DETACHED EDDY SIMULATION (DES); REYNOLDSAVERAGED NAIVER-STOKES (RANS) SOLVER; TIME-SPECTRAL (TS) APPROACH;

AERODYNAMICS;

EID: 35648957707     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-3929     Document Type: Conference Paper

References (40)

1. J. Sitaraman, A. Datta, J. Baeder, and I. Chorpa, "Coupled CFD/CSD Prediction for Rotor Aerodynamic and Structural Dynamic Loads for Three Critical Flight Conditions," 31st European Rotorcraft Forum,Firenze, Italy, 2005.
2. 2P. B. Martin, C. Tung, M.S. Chandrasekhara, and E. Arad. "Active Separation Control: measurements and Computations for a NACA0036 Airfoil," AIAA-2003-3516, 2003.
3. E. Arad, P. B. Martin, J. Wilson, and C. Tung, "Control of Massive Separation on A Thick-Airfoil Wing: A Computational and Experimental Study," 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006.
4. K. D. Squires, "Detached-Eddy Simulation: Current Status and Perspectives," Proceedings of Direct and Large-Eddy Simulation-5, 2004.
5. J. S. Wilson "Turbulence Measurements on a 2D NACA0036 with Synthetic Jet Flow Control," 62nd Annual Forum of the American Helicopter Society, Phoenix, Arizona, May 9-11, 2006.
6. E. van der Weide, G. Kalitzin, G. Schluter, J. J. Alonso, "Unsteady Turbomachinery Computations Using Massively Parallel Platforms," AIAA Paper 2006-0421, Reno, NV, January 2006.
7. P. R. Spalart, and S. R. Allmaras, "A One-Equation Turublence Model for Aerodynamic Flows," AIAA Paper 92-0439, 1992.
8. P. R. Spalart, and S. R. Allmaras, "A One-Equation Turublence Model for Aerodynamic Flows," La Recherche Aerospatiale n1, 5-21, 1994
9. D. C. Wilcox, "Turbulence Modeling for CFD," DCW Industries, Dec, 2002.
10. F. R. Menter, "Two-equation eddy-viscosity turbulence models for engineering applications," AIAA Journal, vol. 32, pp. 269-289, 1994
11. G. Kalitzin, G. Medic, G. Iaccarino, and P. Durbin, "Near-wall behavior of RANS turbulence models and implications for wall functions," Journal of Computational Physics, vol. 204, VV- 265-291, 2005
12. 2 model," AIAA Journal, vol. 33, pp. 659-664, 1995.
13. P. Durbin, "Near wall turbulence closure modleing without damping functions," Theo. Comp. Fluid Dyna. vol.3, 1991.
14. G. Kalitzin, G. Medic, G. Iaccarino and P. Durbin "Near-wall behavior of RANS turbulence models and implications for wall functions," Journal of Computational Physics, Volume 204, Issue 1, pp. 265-291, March 2005.
15. 2 -f turbulence model to tip vortex flows," Center for Turbulence Research Annual Research Briefs, 2005.
16. K. Duraisamy, W. J. McCroskey, J. D. Baeder, "Analysis of Wind Tunnel Wall Interference Effects on Unsteady Subsonic Airfoil Flows," AIAA-2006-2993, Reno, NV, Jan. 2006.
17. B. A. P. Reif, P. Durbin, A. Ooi, "Modeling rotational effects using eddy-viscosity closures," International Journal of Heat Fluid Flow, vol.20, pp. 563-573, 1999.
18. J. S. Chow, G. Zilliac, and P. Bradshaw, "Mean and turbulence measurements in the near field of a wingtip vortex," AIAA Journal, vol. 35, pp. 1561-1567, 1997
19. J. S. Baggett, J. Jimenez, and A. G. Kravchenko, "Resolution requirements in large-eddy simulations of shear flows," Annual Research Briefs, Center for Turbulence Research, NASA Ames/Stanford, 1997
20. G. Kalitzin, J. A. Templeton, and G. Medic, "A near-wall eddy-viscosity formulation for LES.," Symposium on Complex Effects in Large Eddy Simulation, Limassol, Cyprus, 2005
21. P. R. Spalart, W. -H. Jou, M. Stretlets, and S. R. Allmaras, "Comments on the Feasibility of LES for Wings and on the Hybrid RANS/LES Approach," Proceedings of the First AFOSR International Conference on DNS/LES, 1997
22. M. Strelets, "Detached Eddy Simulation of Massively Separated Flows," AlAA 2001-0879
23. A. Jameson, "Time dependent calculations using multigrid, with application to unsteady flows past airfoils and wings," AIAA Journal, 91-1956, June 1998.
24. K. C. Hall, J. P. Thomas, and W. S. Clark. "Computation of unsteady nonlinear flows in cascades using a harmonic balance technique," AIAA Journal, 40(5):879-886, May 2002.
25. M. S. McMullen, "The Application of Non-Linear Frequency Domain Methods To the Euler and Navier-Stokes Equations," Ph. D thesis, Stanford University, March 2003.
26. F. Kachra and S. K. Nadarajah, "Viscous Aeroelastic Solutions Using the Non-Linear Frequency Domain Method," 24th Applied Aerodynamics Conference, June 5-8, San Francisco, California.
27. A. K. Gopinath, and A. Jameson. "Time Spectral Method for Periodic Unsteady Computations over Two- and Three-Dimensional Bodies," AIAA-2005-1220, Jan. 2005.
28. A. K. Gopinath, and A. Jameson "Application of the Time Spectral Method to Periodic Unsteady Vortex Shedding," AIAA-2006-0449, Jan. 2006.
29. E. van der Weide, A. Gopinath, and A. Jameson, "Turbomachinery Applications with the Time Spectral Method," AIAA-2005-4905, Toronto, Canada, June 2005.
30. G. Medic, G. Kalitzin, D. You, E. van der Weide, J. J. Alonso, and H. Pitsch, "Integrated RANS/LES Computations of an Entire Gas Turbine Jet Engine," AIAA Paper 2007-1117, Reno, NV, January 2007.
31. C. Canuto, M. Y. Hussaini, A. Quarteroni, T. A., Jr. Zang "Spectral Methods in Fluid Dynamics," Springer, 1998.
32. K.Lee, J.J.Alonso, and E.v.d.Weide, "Mesh Adaptation Criteria for Unsteady Periodic Flows Using a Discrete Adjoint Time-Spectral Formulation," AIAA-2006-692, Reno, NV, Jan. 9-12, 2006.
33. P. R. Spalart, "Young-Person's Guide to Detached-Eddy Simulation Grids," NASA/CR-2001-211032, 2001.
34. A. R. Piziali "An experimental investigation of 2D and 3D oscillating wing aerodynamcis for a range of angles of attack including stall," NASA TM 4632, 1994.
35. A. Datta, and I. Chopra "Prediction of UH-60A Dynamic Stall Loads in High Altitude Level Flight using CFD/CSD Coupling," 61st Annual Forum of the American Helicopter Society, grapevine, Texas, Junel-3, 2005.
36. Bousman, G. and Kufeld, R.M., Balough, D., Cross, J.L., Studebaker, K.F. and Jennison, CD. "Flight Testing the UH-60A Airloads Aircraft," 50th Annual Forum of the American Helicopter Society, Washington, D.C, May 1994.
37. Kufeld, R. M., and Bousman, W. G. "UH-60A Airloads Program Azimuth Reference Correction," Technical Note, Journal of the American Helicopter Society, Vol.50, No.2, pp.211-213 2005.
38. E. Oran Brigham, "The fast Fourier transform and its applications," Englewood Cliffs, N.J. : Prentice Hall, 1998.
39. M. Potsdam, H. Yeo, and W. Johnson, "Rotor Airloads Prediction Using Loose Aerodynamic/Structural Coupling," Proceedings of the American Helicopter Society 60th Annual Forum,Baltlmore, MD, June 2004.
40. A. Datta, J. Sitaraman, I. Chopra, and J. Baeder, "CFD/CSD Prediction of Rotor Vibratory Loads in High-Speed Flight," Journal of Aircraft, Vol.43, No.6, 2006.