Buzz Margin Control for Supersonic Intake Operating over Wide Range of Mach Number |
Park, Iksoo
(Advanced Propulsion Technology Center, Agency for Defence Development)
Park, Jungwoo (Advanced Propulsion Technology Center, Agency for Defence Development) Lee, Changhyuck (Ant-ship Missile Systems Department, Agency for Defence Development) Hwang, Kiyoung (Advanced Propulsion Technology Center, Agency for Defence Development) |
1 | Hui, O.Y., Zhu, Z.l. and Min, C., "Conceptual Design of Geometry-Variable Hypersonic Intake for TBCC," 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, U.S.A., Jul. 21-23, 2008. |
2 | Guido, K. and Christoph, B., "Air Intake Development for Supersonic Missiles," 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, U.S.A., Jul. 21-23, 2008. |
3 | Park, J.W., Park, I.S., Seo, B.G., Sung, H.G., Ananthkrishinan, N. and Tahk, M.J., "Optimal Terminal Shock Position Under Disturbances for Ramjet Supercritical Operation," Journal of Propulsion and Power, Vol. 29, No. 1, pp. 238-248, 2013. DOI |
4 | Herbert, G. H., "Analysis of Shock Motion in Ducts during Disturbances in Downstream Pressure," NASA TN-4090, 1957. |
5 | Herbert, G.H., George, V. and William, R.D., "Experimental Study of Shock-Positioning Method of Ramjet Engine Control," NACA RM-E55F21, 1955. |
6 | Park, I.S., Kim, S.K., Yeom, H.W., Sung, H.G., Park, J.W. and Tahk, M.J., "Control-Oriented Model for Intake Shock Position Dynamics in Ramjet Engine," Journal of Propulsion and Power, Vol. 27, No. 2, pp. 499-503, 2011. DOI ScienceOn |
7 | Fred, A.W., Eugene, P. and Donald, P.H., Investigation of an on off inlet shock position control on a 16 inch ramjet engine," NACA RM-E54I21, 1954. |
8 | Ohshima, T., Kanbe, K., Kimura, H., Fujiwara, K., Suzuki, K. and Yanagi, R., "Control of the Intake Shock Position in the Test Rig for Ramjet Engine," 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Seattle, WA, U.S.A., Jul. 6-9, 1997. |
9 | Seymour, C.H., "Some Control Considerations for Ram-jet Engines," NACA RM-E52F10, 1952. |
10 | Paul, P. W. and Fred A.W., "Use of Supersonic Diffuser Mach Number as a Supersonic-Inlet Control Parameter," NACA RM-E56F05, 1956. |
11 | Aaron, S.B. and David, N., "Control Requirements and Control Parameters for A Ramjet with Variable-Area Exhaust Nozzle," NACA RM-E8H24, 1948. |
12 | Choi, J.H., Lee, J.Y., Yoon, H.G. and Lim, J.S., "Supersonic Air Data Acquisition Algorithm using Total Pressure Sensors," KSPE Spring Conference, pp. 215-218, 2011. |
13 | Tank, W. and Gillis, J., "Atmospheric Disturbance Models for Linear and Nonlinear System Response Analysis," 34th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, U.S.A., Jan. 15-18, 1996. |