1 |
Lee, J. W., Yee, K. J. and Oh, S. J., "The Aerodynamic Analysis of Helicopter Rotors by Using an Unsteady Source-Doublet Panel Method," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 34, No. 6, 2006, pp. 1~9.
DOI
|
2 |
McClung, A. M., "Development and validation of an unsteady panel code to model airfoil aeromechanical response," M.S. Thesis, Mechanical and Aerospace Engineering Deptartment, Oklahoma State University, 2004.
|
3 |
Erickson, L. L., "Panel methods: An introduction," NASA Technical Paper 2995, 1990.
|
4 |
Hess, J. L., "Calculation of potential flow about arbitrary three-dimensional lifting bodies," McDonnell Douglas Corporation Technical Report No. MDC J5679-01, 1972.
|
5 |
Woodward, F. A., "An improved method for the aerodynamic analysis of wing-body-tail configurations in subsonic and supersonic flow, Part 1- Theory and Applications," NASA Contractor Report 2228 Part 1, 1973.
|
6 |
Maskew, B., "Program VSAERO theory Document: a computer program for calculating nonlinear aerodynamic characteristics of arbitrary configurations," NASA Contractor Report 4023, 1987.
|
7 |
Bristow, D. R. and Hawk, J. D., "Subsonic panel method for designing wing surfaces from pressure distribution," NASA Contractor Report 3713, 1983.
|
8 |
Willis, D. J., "An unsteady, accelerated, high order panel method with vortex particle wakes," Ph.D. Thesis, Aeronautics and Astronautics Dept., Massachusetts Institute of Technology, 2006.
|
9 |
Newman, J. N., "Distributions of sources and normal dipoles over a quadrilateral panel," Journal of Engineering Mathematics, Vol. 20, No. 2, 1986, pp. 113~126.
DOI
|
10 |
John, H. F., "Generic wing, pylon, and moving finned store," Arnold Engineering Development Center (AEDC), Arnold AFB, TN 37389-6001, 2000.
|
11 |
Tai, M. S., Kang, S. O., Oh, S. J. and Park, D. H., "Prediction of Pitching Dynamic Derivatives of Aircraft Using a Unsteady Source Doublet Panel Method," Journal of Computational Fluid Engineering, Vol. 24, No. 1, 2019, pp. 113~123.
DOI
|
12 |
Nathman, J. K. and Matarrese, M., "Hybrid grid (structured and unstructured) calculations with a potential-based panel method," 22nd AIAA Applied Aerodynamics Conference and Exhibit, August 2004, p. 4836.
|
13 |
Kinney, D., "Aero-thermodynamics for conceptual design," 42nd AIAA Aerospace Sciences Meeting and Exhibit, January 2004, p. 31.
|
14 |
Oh, J. A. and Lee, J. T., "Formulation of the Panel Method with Linearly Distributed Dipole Strength on Triangular Panels," Journal of the Society of Naval Architects of Korea, Vol. 57, No. 2, 2020, pp. 114~123.
DOI
|
15 |
Maskew, B., "USAERO/FSP: a time-domain approach to compute free-surface problems," Proceedings of Symposium of High-Speed Marine Vehicles, 1991.
|
16 |
Morino, L., "Steady, Oscillatory, and Unsteady Subsonic and Supersonic Aerodynamics-Production Version (SOUSSA-P 1.1), Volume I-Theoretical Manual," NASA Contractor Report 159130, 1980.
|
17 |
Van Oosterom, A. and Strackee, J., "The solid angle of a plane triangle," IEEE transactions on Biomedical Engineering, Vol. BME-30, No. 2, February 1983, pp. 125~126.
DOI
|
18 |
Baek, C., Lee, S. and Huh, J., "Supersonic Multi-species Jet Interactions of Hit-to-Kill Interceptor with High Temperature Effect," Journal of The Korean Society for Aeronautical and Space Sciences, Vo. 48, No. 3, 2020, pp. 187~194.
DOI
|
19 |
Sleeman, J. and William, C., "An experimental study at high subsonic speeds of several tail configurations on a model with an unswept wing," NACA Research Memorandum L56A06a, 1956.
|
20 |
Giesing, J. P., "Two-dimensional potential flow theory for multiple bodies in small amplitude motion," AIAA Journal, 1970, Vol. 8, No. 11, pp. 1944~1953.
DOI
|
21 |
Ashby, D. L., Dudley, M. R., Iguchi, S. K., Browne, L. and Katz, J., "Potential flow theory and operation guide for the panel code PMARC," NASA Technical Memorandum 102851, 1991.
|
22 |
Carmichael, R. and Erickson, L., "PANAIR-A higher order panel method for predicting subsonic or supersonic linear potential flows about arbitrary configurations," AIAA 14th Fluid and Plasma Dynamics Conference, June 1981, p. 1255.
|