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NTIS 바로가기한국항공우주학회지 = Journal of the Korean Society for Aeronautical & Space Sciences, v.49 no.8, 2021년, pp.609 - 615
이형진 (Dept. of Aerospace and Mechanical Engineering, Graduate School, Korea Aerospace University) , 고상호 (School of Aerospace and Mechanical Engineering, Korea Aerospace University) , 강태곤 (School of Aerospace and Mechanical Engineering, Korea Aerospace University) , 이열 (School of Aerospace and Mechanical Engineering, Korea Aerospace University)
Three-dimensional numerical study was carried out to evaluate the aerodynamic characteristics of the supersonic grid fins installed on SpaceX Falcon 9. The present three-dimensional flow results were compared to the results by the concept of the unit grid fin previously introduced for more efficient...
Belotserkovsky, S. M., Tyulenev, A. I., Odnovol, L. A. and Frolov, V. N., "Reschetchatye Krylya," Moscow, Mashinostroeniye, 1985.
Washington, W. D. and Miller, M. S., "Grid Fins - A New Concept for Missile Stability and Control," 31st Aerospace Science Meeting and Exhibit, January 1993, AIAA 1993-0035.
DeSpirito, J., Edge, H. L., Weinacht, P. and Sahu, J., "Computational Fluid Dynamic Analysis of a Generic Missile with Grid Fins," ARL-TR2318, 2000.
Berner, C. and Dupuis, A., "Wind Tunnel Tests of a Grid Finned Projectile Configuration," 2000, AIAA 2000-0105.
Lin, H., Huang, J. C. and Chieng, C. C., "Navier-Stokes Computations for Body/Cruciform Grid Fin Configuration," Journal of Spacecraft and Rockets, Vol. 40, No. 1, 2003, pp. 30~38.
DeSpirito, J., Vaughn Jr., M. E. and Washington, W. D., "Numerical Investigation of Canard-Controlled Missile with Planar and Grid Fins," Journal of Spacecraft and Rockets, Vol. 40, No. 3, 2003, pp. 363~370.
Burkhalter, J. E., Hartfield, R. J. and Leleux, T. M., "Nonlinear Aerodynamic Analysis of Grid Fin Configurations," Journal of Aircraft, Vol. 32, No. 3, 1995, pp. 547~554.
Theerthamalai, P., "Aerodynamic Characterization of Grid Fins at Subsonic Speeds," Journal of Aircraft, Vol. 44, No. 2, 2007, pp. 694~697.
Ravindra, K., Nikhil, V. S. and Balakrishnan, N., "CFD Simulation of the Grid fin Flows," 2013, AIAA 2013-3023.
Abate, G. L. and Duckerschein, R. P., "Subsonic/Transonic Free-Flight Tests of a Generic Missile with Grid Fins," 2000, AIAA 2000-0937.
Despeyroux, A., Hickey, J. P., Desaulnier, R., Luciano, R., Piotrowski, M. and Hamel, N., "Numerical Analysis of Static and Dynamic Performances of Grid Fin Controlled Missiles," Journal of Spacecraft and Rockets, Vol. 52, No. 4, 2015, pp. 1236~1252.
Huang, C., Liu, W. and Yang, G., "Numerical studies of static aeroelastic effects on grid fin aerodynamic performances," Chinese Journal of Aeronautics, Vol. 30, No. 4, 2017, pp. 1300~1314.
Dikbas, E., Baran, O. U. and Sert, C., "Simplified Numerical Approach for the Prediction of Aerodynamic Forces on Grid Fins," Journal of Spacecraft and Rockets, Vol. 55, No. 4, 2018, pp. 887~898.
SpaceX, https://www.spacex.com, https://www.youtube.com/user/spacexchannel.
Sondak, D. L., "Wall functions for the k-ε turbulence model in generalized nonorthogonal curvilinear coordinates," Ph.D. Thesis, Iowa State University, 1992.
Shih, T. H., Liou, W. W., Shabbir, A., Yang, Z. and Zhu, J., "A New k-ε Eddy-Viscosity Model for High Reynolds Number Turbulent Flows-Model Development and Validation," Computer Fluids, Vol. 24, No. 3, 1995, pp. 227~238.
Roe, P. L., "Approximate Riemann solvers, parameter vectors, and difference schemes," Journal of Computational Physics, Vol. 43, 1981, pp. 357~372
DeSpirito, J., Edge, H. L., Weinacht, P., Sahu, J. and Dinavahi, S. P. G., "Computational Fluid Dynamic Analysis of a Missile with Grid Fins," Journal of Spacecraft and Rockets, Vol. 38, No. 5, 2001, pp. 711~718.
DeSpirito, J., Vaughn, Jr., M. E. and Washington, W. D., "Numerical Investigation of Aerodynamics of Canard-Controlled Missile Using Planar and Grid Tail Fins, Part I: Supersonic Flow," ARL-TR-2848, 2002.
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