1 |
Ferri, A. A. and Nucci, L. M., 1951, "Preliminary Investigation of A New Type of Supersonic Inlet", NACA TN 1104, pp. 1029-1047.
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2 |
Seddon, J. and Goldsmith, E. L., 1999, Intake Aerodynamics-Second Edition, AIAA Education Series, VA, pp. 193-197.
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3 |
Moeckel, W. E., 1949, "Approximate Method for Prediting Form and Location of Detached Shock Waves Ahead of Plane or Axially Symmetric Bodies", NACA TN 1921
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4 |
Osmon, R. V., 1967, "Improved Methods of Spillage Drag Prediction for Two-Dimensional Supersonic Inlets", AIAA Paper 67-449
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5 |
Sibulkin, M., 1951, "Theoretical and Experimental Investigation of Additive Drag", NACA TN 1187, pp. 679-689.
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6 |
Kim, M. G, Jung, S. Y., Byon, W. S. and Lee, K. S., 2010, "The Investigation of Spillage Drag around the Inlet of Air-Breathing Vehicle," Procedings of the 2010 KIMST Conference and Exhibit.
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7 |
Jung, S. Y. and Kim, M. G., 2012, "Numerical Analysis on Supersonic Intake Flow with Back Pressure Condition," Proceedings of the 7th National Congress on Fluids Engineering, Vol. 7, pp. 426-427.
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8 |
Kurth, G. and Bauer, C., 2008, "Air Intake Development for Supersonic Missiles", AIAA-2008-5263, 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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9 |
Lee, J. H., Kim, M. K., and Jung, S. Y., 2014, "Additive drag computation of supersonic inlet by numerical analysis on inviscid flow", Proceedings of the 8th National Congress on Fluids Engineering
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