1 |
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.
|
2 |
Rosema, C. C., Doyle, J. B. and Blake, W. B., Missile Data Compendium (DATCOM) User Manual - 2014 Revision, December 2014.
|
3 |
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.
DOI
|
4 |
Pitts, W. C., Nielsen, J. N. and Kaattari, G. E., "Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic, and Supersonic Speeds," NACA TR-1307, 1957.
|
5 |
Blake, W. B., MISSILE DATCOM User's Manual-2011 Revision, Air Force Research Laboratory, March 2011.
|
6 |
Siemens Industries Digital Software, Simcenter STAR-CCM+ User Guide - Version 2021.6, Siemens, June 2021.
|
7 |
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.
DOI
|
8 |
Roe, P. L., "Approximate Riemann Solvers, Parameter Vectors, and Difference schemes," Journal of Computational Physics, Vol. 43, No. 2, 1981, pp. 357~372.
DOI
|
9 |
Menter, F. R., "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA Journal, Vol. 32, No. 8, 1994, pp. 1598~1605.
DOI
|
10 |
Moore, F., Approximate Methods for Weapon Aerodynamics, AIAA, 2000, pp. 143~149.
|
11 |
Lesieutre, D. J., "MISL3 Aerodynamic Analysis For Finned Vehicles With Axisymmetric Bodies," NEAR TR 654, Nielsen Engineering & Research, June 2010.
|
12 |
Kang, E. J., Go, B. Y. and Lee, K. S., "Analysis for Rolling Moment Characteristics of Canard-Tail Missile using CFD," Proceeding of The Korean Society for Computational Fluids Engineering Spring Conference, May 2018, pp. 90~91.
|
13 |
Yoon, S. J., "Some Trends in Aerodynamic Analysis Methods," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 22, No. 3, 1994, pp. 107~116.
|
14 |
Moore, F. G. and Moore, L. Y., "New Method to Predict Nonlinear Roll Damping Moments," Journal of Spacecraft and Rockets, Vol. 45 No. 5, 2008, pp. 955~964.
DOI
|
15 |
Venkatakrishnan, V., "On the Accuracy of Limiters and Convergence to Steady State Solutions," AIAA 31st Aerospace Sciences Meeting, January 1993.
|
16 |
Blair Jr., A. B., Love, J. and Lesieutre, D., "Recent Applications and Improvements to the Engineering-Level Aerodynamic Prediction Software MISL3," AIAA Paper 2002-0275, AIAA 40th Aerospace Sciences Meeting, January 2002.
|