Abstract
The helicopter aerodynamics is simulated in hovering and forwarding flight using the unsteady Euler equations. As the steady condition, flight test of DLR-F6 and hovering flight test data of Caradonna & Tung’s rotor blades were used, and as the unsteady condition, non-lift forwarding flight test data of the rotor blades were used. The parallelized numerical solver was validated with the two of data above. By using this solver, AH-1G rotor blades to forwarding flight numerical test were conducted. In the test of forwarding flight, the numerical trim was applied to decide cyclic pitching angles using the Newton-Raphson method, and the results were good well match to the experimental data, Especially, the BVI effects were well simulated in advancing side in comparison with other numerical results. To consider the blade motion and moving effects, an overset grid technique is applied and for the boundary, Riemann invariants condition is used for inflow and outflow.
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References
Eugene Kim, J. H. Kwon and S. H. Park, ” Parallel Performance Assessment of Moving Body Overset Grid Application on PC Cluster”, pp59-66, Parallel Computational Fluid Dynamics-Parallel Computing and Its Applications 2007.
S. H. Park, Y. S. Kim and J. H. Kwon, ”Prediction of Damping Coefficients Using the Unsteady Euler Equations”, Journal of Spacecraft and Rockets, Vol.40,No.3,2003,pp.356-362
Y. Kim, S. H. Park and J. H. Kwon, ”Drag Prediction of DLR-F6 Using the Turbulent Navier-Stokes Calculations with Multigrid,” AIAA Paper 2004-0397, 42nd Aerospace Science Meeting and Exhibit, Reno, NV, Jan. 2004.
F. X. Caradonna and C. Tung, ”Experimental and Analytical Studies of a Model Helicopter Rotor in Hover,” NASA TM-81232, Sep. 1981.
F. X. Caradonna, F. X., G. H. Laub and C. Tung, ”An Experimental Investigation of the Parallel Blade-Vortex Interaction,” NASA TM-86005, 1984.
J. L. Cross and M. E. Watts, ”Tip Aerodynamics and Acoustics Test: A Report and Data Survey,” NASA-RP-1179, NASA Ames Research Center, Dec. 1988.
K. H. Chung, C. J. Hwang, Y. M. Park, W. J. Jeon and D. J. Lee, ” Numerical Predictions of Rotorcraft Unsteady air-loadings and BVI noise by using a time-marching free-wake and acoustic analogy”, 31th European Rotorcraft Forum, 2005.
P. L. Roe, ”Approximate Riemann Solver, Parameter Vectors and Differnce Schemes”, Journal of Computational Physics, Vol 43, pp. 357-372, 1981.
A. Harten, ”High Resolution Schemes for Hyperbolic Conservation Laws,” Journal of Computational Physics, Vol. 49, pp.357-393, 1983.
W. K. Anderson, J. L. Tomas, and B. Van Leer, ”Comparison of Finite Volume Flux Vector Splittings for the Euler Equations,” AIAA Journal, Vol. 24, No. 9, pp. 1453-1460. 1986.
T. Pulliam and D. chaussee, ” A diagonal form of an implicit approximate-factorization algorithm”, Journal of Computational Physics, Vol. 39, pp. 347-363, 1981.
K. W. Cho, J. H. Kwon, and S. Lee., ”Development of a Fully Systemized Chimera Methodology for Steady/Unsteady Problems”, Journal of Aircraft, Vol. 36, No. 6, pp. 973-980, Nov. Dec. 1999
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Im, DK. et al. (2010). Aerodynamic Analysis of Rotor Blades using Overset Grid with Parallel Computation. In: Tromeur-Dervout, D., Brenner, G., Emerson, D., Erhel, J. (eds) Parallel Computational Fluid Dynamics 2008. Lecture Notes in Computational Science and Engineering, vol 74. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-14438-7_10
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DOI: https://doi.org/10.1007/978-3-642-14438-7_10
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