참고문헌
- Sturek, W.B., Nietubicz, C.J., Sahu, J., and Weinacht, P., "Applications of Computational Fluid Dynamics to the Aerodynamics of Army Projectiles," J. Space. Rockets, Vol. 31, No. 2, 1994, pp. 186-199. https://doi.org/10.2514/3.26422
- 박수형, 권장혁, 허기훈, 변우식, “천음속 미사일의 동안정성에 대한 충격파 영향,” 한국항공우주학회지, 30권 2호, 2002, pp. 12-20. https://doi.org/10.5139/JKSAS.2002.30.2.012
- Park, S.H., Kim, Y., and Kwon, J.H., "Prediction of Damping Coefficients Using the Unsteady Euler Equations," J. Space. Rockets, Vol. 40, No. 3, 2003, pp. 356-362. https://doi.org/10.2514/2.3970
- Tobak, M., and Schiff, L.B., "Generalized Formulation of Nonlinear Pitch-Yaw-Roll Coupling," AIAA J., Vol. 13, No. 3, 1975, pp. 323-332. https://doi.org/10.2514/3.49698
- Schiff, L.B., "Nonlinear Aerodynamics of Bodies in Coning Motion," AIAA J., Vol. 10, No. 11, 1972, pp. 1517-1522. https://doi.org/10.2514/3.50395
- Weinacht, P., Sturek, W.B., and Schiff L.B., "Navier-Stokes Predictions of Pitch Damping for Axisymmetric Projectiles," J. Space. Rockets, Vol. 34. No. 6, 1997, pp. 753-761. https://doi.org/10.2514/2.3306
- Weinacht, P., "Navier-Stokes Predictions of the Individual Components of the Pitch-Damping Sum," J. Space. Rockets, Vol. 35. No. 5, 1998, pp. 598-605. https://doi.org/10.2514/2.3390
- Qin, N., Ludlow, D.K., Shaw, S.T., Edwards, J.A., and Dupuis, A., "Calculation of Pitch Damping Coefficients for Projectiles," AIAA paper 97-0405, Jan. 1997.
- Park, S.H., and Kwon, J.H., "Comparisons of Steady and Unsteady Methods for Pitch-Damping Predictions," AIAA paper 2003-3671, June 2003.
- 허기훈, 윤성준, “회전 유도탄의 롤 댐핑 모멘트에 관한 수치적 연구,” 제 9차 유도무기 학술대회, 국방과학연구소, pp. 24-31.
- Dubuc, L., Cantariti, F., Woodgate, M., Gribben, B., Badcock, K.J., and Richard, B.E., "Solution of the Unsteady Euler Equations Using an Implicit Dual-Time Method," AIAA J., Vol. 36, No. 8, 1998, pp. 1417-1424. https://doi.org/10.2514/2.532
- 박수형, 성춘호, 권장혁, “압축성 유동에 대한 다중격자 DADI 기법의 수렴성 연구,” 한국항공우주학회지 29권 5호, 2001, pp. 25-32.
- Park, T.S., and Kwon, J.H., "An Improved Multistage Time Stepping for Second-order Upwind TVD Schemes," Computers & Fluids, Vol. 25, No. 7, 1996, pp. 629-646. https://doi.org/10.1016/0045-7930(96)00014-X
- Moore, F.G., and Swanson, R.C., "Dynamic Derivatives for Missile Configurations to Mach Number Three," J. Space. Rockets, Vol. 15, No. 2, 1978, pp. 65-66. https://doi.org/10.2514/3.57289