참고문헌 (13)

1. Chin, S. S., Missile Configuration Design, McGraw-Hill, 1961. 

2. Monta, W. J., "Supersonic Aerodynamic Characteristics of a Sparrow III Type Missile Model with Wing Controls and Comparison with Existing Tail-Control Results," NASA TP 1087, 1977. 

3. Cho, T. H., Kim, M. D. and Hyun, J. S., "Wind Tunnel Investigation of the Effect of Lifting Surface Shapes on a Wing-Body-Tail Missile at Supersonic Speed," International Conference on Method and Means for Experimental Investigation in Aerodynamics, Russia, 1993. 

4. Han, M. S., Myong, R. S., Cho, T. H., Hwang, J. S. and Park, C. H., "Analysis of the Aerodynamic Characteristics of Missile Configurations Using a Semi-Empirical Method," Journal of the Korean Society for Aeronautical and Space Sciences, 2005.3, pp. 26-31 

5. Blake, W. B., "MISSILE DATCOM User's manual-1997 Fortran 90 Revision," Air Force Research Laboratory, February 1998. 

6. Yoon, S. J., "Some Trends in Aerodynamic Analysis Methods," Journal of the Korean Society for Aeronautical and Space Sciences, 1994, pp. 107-116. 

7. Thomas, J. S. and Rebecca, Z. S., "Aerodynamic Predictions, Comparisons, and Validations Using Missile DATCOM(97) and Aeroprediction 98 (AP98)," Journal of Spacecraft and Rockets, Vol. 42, No. 2, 2005, pp. 257-265 

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8. Kim, D. H., Lee, D. Y., Kang, D. G. and Lee, H. J., "A wing-tail interference for a tail-controlled missile," Journal of the Korean Society for Aeronautical and Space Sciences, 2017, pp. 817-824. 

9. Moore, F. G. and Moore, L. Y., "2009 Version of the Aeroprediction Code: AP09," Journal of Spacecraft and Rockets, Vol. 45, No. 4, 2008, pp. 677-690 

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10. Moore, F. G. and Moore, L. Y., "Approximate Method to Calculate Nonlinear Rolling Moment due to Differential Fin Deflection," Journal of Spacecraft and Rockets, Vol. 49, No. 2, 2012, pp. 250-260. 

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11. Graves, E. B. and Fournier, R. H., "Stability and Control Characteristics at Mach Numbers from 0.20 to 4.63 of a Cruciform Air-to-Air Missile with Triangular Canard Controls and a Trapezoidal Wing," NASA TM X-3070, 1974. 

12. Blair, A. B., Allen, J. M. and Hernandez, G., "Effect of Tail-Fin Span on Stability and Control Characteristics of a Canard-Controlled Missile at Supersonic Mach Numbers," NASA TP 2157, 1893. 

13. Hemsch, M. J., "The Component Build-Up Method for Engineering Analysis of Missiles at Low-to-High Angles of Attack," Tactical Missile Aerodynamics: Prediction Methodology, AIAA, 1992.