1 |
Kang, D. W., Kim, J. W., Myong, R. S. and Kim, W. C., "Computational investigation of the effect of UAV engine nozzle configuration on infrared signature," Journal of Korean Society for Aeronautical and Space Science, Vol. 41, No. 10, 2013, pp. 779~787.
DOI
|
2 |
Lee J. H., Lee H. J., Yang B. J., Myong R. S. and Kim W. C., "Numerical analysis of thermal flow field according to shape of exhaust nozzle of UCAV and jet on/off," Journal of Computational Fluids Engineerings, Vol. 23, No. 1, 2018, pp. 77~85.
DOI
|
3 |
Lee, H. J., Lee, J. H., Myong, R. S., Kim, S. M., Choi, S. M. and Kim, W. C., "Computational and experimental investigation of thermal flow field of micro turbojet engine with various nozzle configurations," Journal of The Korean Society for Aeronautical and Space Science, Vol. 46, No. 2, 2018, pp. 150~158.
|
4 |
Tompson, J. and Birk, A. M., "Design of an infrared signature suppressor for the Bell 205 (UH-1H) helicopter Part 1: aerothermal design," 11th CASI Propulsion Symposium, 2010.
|
5 |
Sun, X., Wang, Z., Zhou, L., Shi, J. and Liu, Z., "Experimental and computational investigation of double serpentine nozzle," Journal of Aerospace Engineering, Vol. 229, No. 11, 2015, pp. 2035~2050.
|
6 |
Ball, R., The Fundamental of Aircraft Combat Survivability: Analysis and Design, American Institute of Aeronautics and Astronautics, 2003.
|
7 |
Mahulikar, S. P., Hemant, R. S. and Arvind, R., "Infrared signature studies of aerospace vehicles," Progress in Aerospace Science, Vol. 43, 2007, pp. 218~245.
DOI
|
8 |
Scott, H., Dennis, K. M. and Morris, P. J., "Aft deck effects on the aeroacoustics of dual stream supersonic jets," AIAA Scitech 2020 Forum, 2020, pp. 1249~1267.
|
9 |
Chen, W., Wang, Z., Zhou, L., Sun, X. and Shi, J., "Influences of shield ratio on the infrared signature of serpentine nozzle," Journal of Aerospace Science and Technology, Vol. 71, 2017, pp. 1~13.
DOI
|
10 |
Shan, Y., Zhou, X., Tan, X., Zhang, J. and Wu, Y., "Parametric design method and performance analysis of double S-shaped nozzles," International Journal of Aerospace Engineering, Vol. 2019, 2019, pp. 1~24.
|
11 |
Sun, P., Zhou, L., Wang, Z. and Sun, X., "Effect of serpentine nozzle on bypass ratio of turbofan engine exhaust," Joint Propulsion Conference, 2018, pp. 4744~4758.
|
12 |
Lee, H. J., An, C. H., Myong, R. S., Choi, S. M. and Kim, W. C., "Computational investigation of nozzle flowfield in a micro turbojet engine and its scaling characteristics," Journal of Computational Fluids Engineering, Vol. 22, No. 1, 2017, pp. 43~50.
DOI
|
13 |
Lee, J. H., Lee, H. J., Myong, R. S., Choi, S. M. and Kim, W. C., "Investigation of IR survivability of unmanned combat aerial vehicle against surface-to-air missile," Journal of The Korean Society for Aeronautical and Space Science, Vol. 45, No. 12, 2017, pp. 1084~1093.
|
14 |
Chae, J. H., Lee, J. W., Ha, N. K., Kim, D. G., Jang, H. S. and Myong, R. S., "Computational analysis of effects of thermal flow field and chemical components on the IR signature in the exhaust plume of a micro jet engine," Journal of Computational Fluids Engineering, Vol. 24, No. 3, 2019, pp. 101~111.
DOI
|
15 |
Heikel, J., Electronic Warfare Self-protection of Battlefield Helicopters: A Holistic View, Ph.D. Dissertation, Helsinki University of Technology, 2005.
|
16 |
White, J. R., Aircraft Infrared Principles, Signatures, Threats, and Countermeasures, Naval Air Warfare Center Weapons Division, No. NAWCWDTP-8773, 2012.
|
17 |
Arvind, R. G., Buijtenen, J. P. and Mahulikar, S. P., "The effect bypass ratio on aircraft plume infrared signatures," AIAA ISBE-1194, 2009.
|
18 |
An, C. H., Kang, D. W., Baek, S. T. and Myong, R. S., "Analysis of plume infrared signatures of S-shaped nozzle configurations of aerial vehicles," Journal of Aircraft, Vol. 53, No. 6, 2016, pp. 1768~1778.
DOI
|
19 |
ANSYS Fluent 2019 R2 User's Guide, ANSYS Inc., 2019.
|
20 |
Park, G. S., Kim, S. M., Choi, S. M., Myong, R. S. and Kim, W. C., "Experimental study of a micro turbo jet engine performance and IR signal with nozzle configuration," Journal of the Korean Society of Propulsion Engineers, Vol. 20, No. 5, 2016, pp. 1~8.
DOI
|