Browse > Article
http://dx.doi.org/10.5139/JKSAS.2020.48.9.725

Acoustic Analysis of Exhaust Supersonic Jet From a Rocket Motor Using 2-D Axis-symmetric Computational Analysis  

Yang, Young-Rok (Agency for Defense Development)
Jeon, Hyuck-Soo (Agency for Defense Development)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.48, no.9, 2020 , pp. 725-730 More about this Journal
Abstract
This study was conducted to reduce the computation time required for the computational acoustic analysis of the supersonic rocket jet plume. In order to reduce the computation time, computational acoustic analysis was performed assuming that the supersonic jet plume is a two-dimensional axis-symmetric problem. The results of computational acoustic analysis showed similar results to the acoustic load measurement results. Through this study, it was confirmed that the acoustic load prediction of the supersonic rocket jet plume can be predicted using a two-dimensional axis-symmetric computational analysis.
Keywords
Computational Acoustic Analysis; Direct Noise Simulation; Super Sonic Jet Noise;
Citations & Related Records
연도 인용수 순위
  • Reference
1 Tam, C. K. W., "Computational aeroacoustics: Issues and methods," AIAA Journal, Vol. 33, No. 10, 1995, pp. 1788-1796.   DOI
2 Tam, C. K. W., "Computational aeroacoustics: An Overview of Computational Challenges and Applications," International Journal of Computational Fluid Dynamics, Vol. 18, No. 6, 2004, pp. 547-567.   DOI
3 Tam, C. K. W., Computational Aeroacoustics, Cambridge, 2012, pp. 21-26.
4 Orszag, S. A., "Analytical theories of turbulence," Journal of Fluid Mechanics, Vol. 41, No. 2, 1970, pp. 363-386.   DOI
5 Mankbadi, R. R., Shih, S. H., Hixon, D. R. and Povinelli, L. A., "Direct Computation of Jet Noise Produced by Large-Scale Axisymmetric Structures," AIAA Journal of Propulsion and Power, Vol. 15, No. 5, 1999, pp. 207-215.
6 Spalart, P. R., "Detached-eddy simulation," Annual review of fluid mechanics, Vol. 41, 2009, pp. 181-202.   DOI
7 Eldred, K. M. and Jones, G. W., Jr., "Acoustic load generated by the propulsion system," NASA SP-8072, 1971, pp. 1-49.
8 Dewan, Y., Golubev, V. V., Lyrintzis, A. S. and Mankdai, R. R., "Detached Eddy simulations of supersonic jets impinging on flat plates," 43rd Fluid Dynamics Conference, 2013.
9 Tsutsumi, S., Ishii, T., Ui, K. and Tokudome, S., "Assessing Prediction and Reduction Technique of Lift-off Acoustics Using Epsilon Flight Data," 53rd AIAA Aerospace Sciences Meeting, 2015, pp. 1-13.
10 Fukuda, K., Tsutsumi, S., Fujii, K., Ui, K., Ishii, T., Oinuma, H., Kazawa, J. and Minesugi, K., "Acoustic measurement and prediction of solid rockets in static firing tests," 15th AIAA/CEAS Aeroacoustics Conference, 2009, pp. 1-13.
11 Kurabayashi, H., Sato, A., Yamashita, K., Nakayama, H., Hori, K., Honda, M. and Hasegawa, K., "Ultrasonic Measurements of Burning Rates in Full-size Rocket Motors," Progress in Propulsion Physics 2, 2011, pp. 135-148.
12 Tsutsumi, S., Ishii, T., Ui, K., Tokudome, S. and Wada, K., "Study on Acoustic Prediction and Reduction of Epsilon Launch Vehicle at Liftoff," Journal of Spacecraft and Rockets, Vol. 52, No. 2, 2015, pp. 350-361.   DOI
13 Van Leer, B., Flux-Vector Splitting for the Euler Equation, Springer Berlin Heidelberg, 1997, pp. 80-89.
14 Chakravarthy, S., Harten, A. and Osher, S., "Essentially non-oscillatory shock-capturing schemes of arbitrarily-high accuracy," 24th Aerospace Sciences Meeting, 1986, p. 339.
15 Sutherland, W., "The Viscosity of Gases and Molecular Force," Philosophical Magazine, S. 5, Vol. 36, 1893, pp. 507-531.   DOI