1 |
Hender, D. R., Gunkel, R. J., 'A Miniature Version of The JA70 Aerodynamic Heating Computer Program, H800(MINIVER)', McDonnel Douglas, June 1970
|
2 |
선철, 안창수, '초음속 유도탄 공력가열 예측', 한국전산유체공학회 춘계학술대회, 2007
|
3 |
Thompson, M. J., 'A Note on the Calculation of Oblique Shock Wave Characteristics', J. of the Aeronautical Science, Nov. 1950
|
4 |
DiCristina, V., 'Three-Dimensional Laminar Boundary Layer Transition on a Sharp 8o Cone at Mach 10', AIAA Journal, Vol. 8, No. 5, pp. 852-856, 1970
DOI
|
5 |
Eckert, E. R. G., 'Survey of Boundary Heat Transfer at High Velocity and High Temperature', WADC, Tech Report 59-624, Apr. 1960
|
6 |
Morgan, V. T., ' The Overall Convective Heat Transfer from Smooth Circular Cylinder", in T. F. Irvine and J. P. Hartnett, Eds., Advances in Heat Transfer, Vol. 11, Academic Press, New York, pp. 199-264, 1975
|
7 |
DeJarnette, F. R. and Ford, C. P., 'Calculation of Pressure on Bodies at Low Angles of Attack in Supersonic Flow', J. of Spacecraft, Vol. 17, No. 6, Nov-Dec. 1980
|
8 |
Syvertson, C. A. and Dennis, D. H., 'A Second-Order Shock Expansion Method Applicable to Bodies of Revolution Near Zero Lift', NACA Report 1328, 1957
|
9 |
Engel, C. D., 'Miniver Upgrade for the AVID System, Vol. 1 : Lanmin User's Manual', NASA Contractor Report 172212, 1983
|
10 |
Jackson, C. M., Jr., Sawyer, W. C. and Smith, R. S., 'A Method for Determining Surface Pressure on Blunt Bodies of Revolution at Small Angles of Attack in Supersonic Flow', NASA TN D-4865, 1968
|
11 |
Anderson, D. A., Tannehill, J. C. and Pletcher, R. H., 'Computational Fluid Mechanics and Heat Transfer', McGraw-Hill Book Company, 1984
|