[KSCI] Korea Science Citation Index Service

http://dx.doi.org/10.5139/IJASS.2017.18.1.70

Coupled Analysis of Thermo-Fluid-Flexible Multi-body Dynamics of a Two-Dimensional Engine Nozzle

Eun, WonJong (Department of Mechanical and Aerospace Engineering, Seoul National University)
Kim, JaeWon (Korea Advanced Institute of Science and Technology)
Kwon, Oh-Joon (Korea Advanced Institute of Science and Technology)
Chung, Chanhoon (Korea Aerospace Industries)
Shin, Sang-Joon (Department of Mechanical and Aerospace Engineering, Seoul National University)
Bauchau, Olivier A. (University of Maryland)

Publication Information

International Journal of Aeronautical and Space Sciences / v.18, no.1, 2017 , pp. 70-81 More about this Journal

Abstract

Various components of an engine nozzle are modeled as flexible multi-body components that are operated under high temperature and pressure. In this paper, in order to predict complex behavior of an engine nozzle, thermo-fluid-flexible multi-body dynamics coupled analysis framework was developed. Temperature and pressure on the nozzle wall were obtained by the steady-state flow analysis for a two-dimensional nozzle. The pressure and temperature-dependent material properties were delivered to the flexible multi-body dynamics analysis. Then the deflection and strain distribution for a nozzle configuration was obtained. Heat conduction and thermal analyses were done using MSC.NASTRAN. The present framework was validated for a simple nozzle configuration by using a one-way coupled analysis. A two-way coupled analysis was also performed for the simple nozzle with an arbitrary joint clearance, and an asymmetric flow was observed. Finally, the total strain result for a realistic nozzle configuration was obtained using the one-way and two-way coupled analyses.

Keywords

Multi-body dynamics; Fluid- flexible multi-body dynamics coupled analysis; Coupled analysis framework;

Citations & Related Records

Times Cited By KSCI : 2 (Citation Analysis)

Reference
Cited By KSCI

1	https://grabcad.com/library/after-burner-nozzle-thrust -vectoring-nozzle-1
2	Whitaker, K. W. and Gowadia, N. S. "Aircraft Thrust Vectoring Using Flexible Nonaxisymmetric Nozzles", Journal of Aircraft, Vol. 31, No. 4, 1994, pp. 984-986. DOI:10.2514/3.46592 DOI
3	Schwane, R. and Xia, Y., "Investigation of Nozzle Stability by Numerical Fluid Structure Interaction Calculation", Proceeding of the 43rd AIAA Aerospace Science Meeting and Exhibit, Reno, NV, 2005.
4	Murugappan, S., Gurmark, E. J., Lakhamraju, R. R. and Khosla, S., "Flow-Structure Interaction Effects on a Jet Emanating from a Flexible Nozzle", Physics of Fluids, Vol. 20, No. 11, 2008, pp. 117105. DOI:10.1063/1.3013634 DOI
5	Wang, T. S., Zhao, X., Zhang, S. and Chen, Y. S., "Development of an Aeroelastic Modeling Capability for Transient Nozzle Floe Analysis", Journal of Propulsion and Power, Vol. 30, No. 6, 2014, pp. 1692-1700. DOI:10.2514/1. B35277 DOI
6	http://www.mscsoftware.com/product/adams
7	http://www.lmsintl.com/DADS
8	Wasfy, T. M., Modeling Flexible Multi-Body Systems Including Impact and Thermal Effects Using the Finite Element Method and Convected coordinates, Ph.D. Dissertation, Columbia University, 1994.
9	http://eng.functionbay.co.kr/
10	Bauchau, O. A., DYMORE User's Manual, School of Aerospace Engineering, Georgia In stitute of Technology, 2006.
11	Mathur, S. R. and Murthy, J. Y., "A Pressure-Based Method for Unstructured Meshes", Numerical Heat Transfer, Part B: Fundamentals, Vol. 31, No. 2, 1997, pp. 195-215. DOI:10.1080/10407799708915105 DOI
12	Kim, J. W. and Kwon, O. J., "Numerical Study of Variable Geometry Nozzle Flow Using a Mesh Deformation Technique on Hybrid Unstructured Meshes", Journal of Computational Fluids Engineering, Vol. 18, No. 3, 2013, pp. 26-33. DOI:10.6112/kscfe.2013.18.3.026 DOI
13	Jung, M. S., Kwon, O. J. and Kang, H. J., "Assessment of Rotor Hover Performance Using a Node-Based Flow Solver", International Journal of Aeronautical and Space Sciences, Vol. 8, No. 2, 2007, pp. 44-53. DOI:10.5139/IJASS.2007.8.2.044 DOI
14	Roe, P. L., "Approximate Riemann Solvers, Parameter Vectors and Difference", Journal of Computational Physics, Vol. 43, No. 2, 1981, pp. 357-372. DOI:10.1016/0021- 9991(81)90128-5 DOI
15	Spalart, P. R. and Allmaras, S. R., "A One-Equation Turbulent Model for Aerodynamic Flows", Proceedings of the 30th Aerospace Sciences Meeting and Exhibit, Reno, NV, 1992.
16	http://www.mscsoftware.com/product/msc-nastran
17	Anonymous, MIL-HDBK-5H: Metallic Materials and Elements for Aerospace Vehicle Structures, U.S. Department of Defense, 2003.
18	Johnson, D. and Mar, H. M., Variable jet propulsion nozzle, Patent, US 3612400A, 1971.
19	Hunter, C. A., "Experimental, Theoretical, and Computational Investigation of Separated Nozzle Flows", Proceedings of the 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, H, 1998.