1 |
Fry, R. S., "A century of Ramjet Propulsion Technology Evolution," Journal of Propulsion and Power, Vol. 20, No. 1, 2004, pp. 27~58.
DOI
|
2 |
Moses, P. L., Rausch, V. L., Nguyen, L. T. and Hill, J. R., "NASA hypersonic flight demonstrators-overview, status, and future plans," Acta astrounautica, Vol. 55, Issues 3-9, 2004, pp. 619~630.
DOI
|
3 |
Won, S. H., Jeung, I. S. and Choi, J. Y., "Overview on Hypersonic Scramjet Engine Developments," Journal of Korean Society of Propulsion Engineers, Vol. 9, No. 1, 2005, pp. 67~83.
|
4 |
Walker, J. J., "Internal Drag Coefficient Correction," General Dynamics Corporation Fort Worth Division, 1980, pp. 1~7.
|
5 |
Kim, J. M. and Lee, Y. B., "A Study on Effective Correction of Internal Drag and Wall Interference Using Response Surface in Wind Tunnel Test," Journal of the Korea Institute of Military Science and Technology, Vol. 22, No. 5, 2019, pp. 637~643.
DOI
|
6 |
Bobbitt, P. J., Maglieri. D. J., Banks, D. W. and Fuchs, A. W., "Wedge and Conical Probes for the Instantaneous Measurement of Free-Stream Flow Quantities at Supersonic Speeds," AIAA-2011-3501, 29th AiAA Applied Aerodynamics Conference, Honolulu, Hawaii, 27-30, June 2011.
|
7 |
Lassaline, J. V., "Supersonic Right Circular Cone at Zero Angle of Attack," High-Speed Aerodynamics, Ryerson University, March, 2009, pp. 1~3.
|
8 |
AIAA Standard, "Assessment of Experimental Uncertainty with Application to Wind Tunnel Testing," AIAA S-071A-1999, 1999.
|
9 |
Marimon, M. M., "Study of an air-breathing engine for hypersonic flight," 2013.
|
10 |
Haberle, J. and Gulhan, A., "Investigation of the Performance of a Scramjet Inlet at Mach 6 with Bopundary Layer Bleed," AIAA 2006-8139, 14th AIAA Space Planes and Hypersonic Systems and Technologies Conference, 2006.
|
11 |
Kim, S. H., Kim, Y. J., Lee, J. G. and Kim, N. G., "Introduction of ADD Hypersonic Wind Tunnels," Proceeding of The Korean Society for Aeronautical and Space Sciences Spring Conference, November 2017, pp. 23~25.
|
12 |
Haberle, J. and Gulhan, A., "Exprimental Investigation of a Two-Dimensional and a Three Dimensional Scramjet Inlet at Mach 7," Journal of Propulsion and Power, Vol. 24, No. 5, SeptemberOctober, 2008, pp. 1023~1034.
DOI
|
13 |
Herrmann, C. D. and Koschel, W. W., "Exprimental Investigation of the Internal Compression of a Hypersonic Intake," AIAA-2002-4130, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 7-10, July, 2002.
|