전산 유체 역학 (Korean Wikipedia)

Analysis of information sources in references of the Wikipedia article "전산 유체 역학" in Korean language version.

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calpoly.edu

digitalcommons.calpoly.edu

Marshall, D., and Ruffin, S.M., " An Embedded Boundary Cartesian Grid Scheme for Viscous Flows using a New Viscous Wall Boundary Condition Treatment,” AIAA Paper 2004-0581, presented at the AIAA 42nd Aerospace Sciences Meeting, January 2004.

doi.org

dx.doi.org

Hess, J.L.; A.M.O. Smith (1967). “Calculation of Potential Flow About Arbitrary Bodies”. 《Progress in Aerospace Sciences》 8: 1–138. Bibcode:1967PrAeS...8....1H. doi:10.1016/0376-0421(67)90003-6.
Rubbert, P.; Saaris, G. (1972). 〈Review and evaluation of a three-dimensional lifting potential flow computational method for arbitrary configurations〉. 《10th Aerospace Sciences Meeting》. doi:10.2514/6.1972-188.
Carmichael, R.; Erickson, L. (1981). 〈PAN AIR - A higher order panel method for predicting subsonic or supersonic linear potential flows about arbitrary configurations〉. 《14th Fluid and Plasma Dynamics Conference》. doi:10.2514/6.1981-1255.
Youngren, H.; Bouchard, E.; Coopersmith, R.; Miranda, L. (1983). 〈Comparison of panel method formulations and its influence on the development of QUADPAN, an advanced low-order method〉. 《Applied Aerodynamics Conference》. doi:10.2514/6.1983-1827.
Hess, J.; Friedman, D. (1983). 〈Analysis of complex inlet configurations using a higher-order panel method〉. 《Applied Aerodynamics Conference》. doi:10.2514/6.1983-1828.
Katz, Joseph; Maskew, Rian (1988). “Unsteady low-speed aerodynamic model for complete aircraft configurations”. 《Journal of Aircraft》 25 (4): 302–310. doi:10.2514/3.45564.
Maskew, Brian (1982). “Prediction of Subsonic Aerodynamic Characteristics: A Case for Low-Order Panel Methods”. 《Journal of Aircraft》 19 (2): 157–163. doi:10.2514/3.57369.
Boppe, C. (1977). 〈Calculation of transonic wing flows by grid embedding〉. 《15th Aerospace Sciences Meeting》. doi:10.2514/6.1977-207.
Samant, S.; Bussoletti, J.; Johnson, F.; Burkhart, R.; Everson, B.; Melvin, R.; Young, D.; Erickson, L.; Madson, M. (1987). 〈TRANAIR - A computer code for transonic analyses of arbitrary configurations〉. 《25th AIAA Aerospace Sciences Meeting》. doi:10.2514/6.1987-34.
Raj, Pradeep; Brennan, James E. (1989). “Improvements to an Euler aerodynamic method for transonic flow analysis”. 《Journal of Aircraft》 26: 13–20. doi:10.2514/3.45717.
Melton, John; Berger, Marsha; Aftosmis, Michael; Wong, Michael (1995). 〈3D applications of a Cartesian grid Euler method〉. 《33rd Aerospace Sciences Meeting and Exhibit》. doi:10.2514/6.1995-853.
Karman, l. (1995). 〈SPLITFLOW - A 3D unstructured Cartesian/prismatic grid CFD code for complex geometries〉. 《33rd Aerospace Sciences Meeting and Exhibit》. doi:10.2514/6.1995-343.
Jameson, A.; Baker, T.; Weatherill, N. (1986). 〈Calculation of Inviscid Transonic Flow over a Complete Aircraft〉. 《24th Aerospace Sciences Meeting》. doi:10.2514/6.1986-103.
Giles, M.; Drela, M.; Thompkins, Jr, W. (1985). 〈Newton solution of direct and inverse transonic Euler equations〉. 《7th Computational Physics Conference》. doi:10.2514/6.1985-1530.
Drela, Mark (1990). 〈Newton solution of coupled viscous/inviscid multielement airfoil flows〉. 《21st Fluid Dynamics, Plasma Dynamics and Lasers Conference》. doi:10.2514/6.1990-1470.

dtic.mil

Woodward, F.A., Dvorak, F.A. and Geller, E.W., "A Computer Program for Three-Dimensional Lifting Bodies in Subsonic Inviscid Flow 보관됨 2019-12-10 - 웨이백 머신," USAAMRDL Technical Report, TR 74-18, Ft. Eustis, Virginia, April 1974.

gatech.edu

ae.gatech.edu

Daniel Guggenheim School of Aerospace Engineering. “NASCART”. 2007년 8월 20일에 원본 문서에서 보존된 문서. 2009년 3월 10일에 확인함.

harvard.edu

adsabs.harvard.edu

Hess, J.L.; A.M.O. Smith (1967). “Calculation of Potential Flow About Arbitrary Bodies”. 《Progress in Aerospace Sciences》 8: 1–138. Bibcode:1967PrAeS...8....1H. doi:10.1016/0376-0421(67)90003-6.

mit.edu

web.mit.edu

Drela, Mark, "XFOIL: An Analysis and Design System for Low Reynolds Number Airfoils," in Springer-Verlag Lecture Notes in Engineering, No. 54, 1989.

nasa.gov

ntrs.nasa.gov

Bristow, D.R., "Development of Panel Methods for Subsonic Analysis and Design," NASA CR-3234, 1980.
Ashby, Dale L.; Dudley, Michael R.; Iguchi, Steve K.; Browne, Lindsey and Katz, Joseph, “Potential Flow Theory and Operation Guide for the Panel Code PMARC”, NASA NASA-TM-102851 1991.
Maskew, Brian, “Program VSAERO Theory Document: A Computer Program for Calculating Nonlinear Aerodynamic Characteristics of Arbitrary Configurations”, NASA CR-4023, 1987.
Eppler, R.; Somers, D. M., "A Computer Program for the Design and Analysis of Low-Speed Airfoils," NASA TM-80210, 1980.
Mead, H. R.; Melnik, R. E., "GRUMFOIL: A computer code for the viscous transonic flow over airfoils," NASA CR-3806, 1985.

psu.edu

citeseerx.ist.psu.edu

Jameson, A., Schmidt, W. and Turkel, E., "Numerical Solution of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes," AIAA paper 81-1259, presented at the AIAA 14th Fluid and Plasma Dynamics Conference, Palo Alto California, 1981.

researchgate.net

Jameson A. and Caughey D., "A Finite Volume Method for Transonic Potential Flow Calculations," AIAA paper 77-635, presented at the Third AIAA Computational Fluid Dynamics Conference, Albuquerque New Mexico, June 1977.

web.archive.org

Woodward, F.A., Dvorak, F.A. and Geller, E.W., "A Computer Program for Three-Dimensional Lifting Bodies in Subsonic Inviscid Flow 보관됨 2019-12-10 - 웨이백 머신," USAAMRDL Technical Report, TR 74-18, Ft. Eustis, Virginia, April 1974.
Daniel Guggenheim School of Aerospace Engineering. “NASCART”. 2007년 8월 20일에 원본 문서에서 보존된 문서. 2009년 3월 10일에 확인함.