Technical Notes
Jan 6, 2021

Numerical Modeling of Fluid Transients with Structural Compliance

Publication: Journal of Aerospace Engineering
Volume 34, Issue 2

Abstract

This paper presents fluid transients in a pipeline with the sudden opening of a valve using a network flow solver based on the finite-volume method. There is entrapped air downstream of the valve. The mathematical model is formulated by integrating the flow equations in the liquid (water) zone and compressibility of the entrapped air and the structural deformation of the pipe. An earlier study by the authors shows a good agreement of computed results using the rigid pipe assumption with the experimental data when the percentage of entrapped air is reasonably high (about 50%). However, as the pressure amplitudes go higher when there is a relatively low volume of entrapped air present, the computed results differ from experimental data both in the amplitude of the pressure oscillations and corresponding frequencies. The use of structural deformation modeling coupled with the fluid dynamics problem reduces the difference for much better comparisons with the experimental data.

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Data Availability Statement

Some or all data, models, or code generated or used during the study are available from the corresponding author by request. Specifically, any data related to the plots and the theory used in the model can be shared. Regarding the computational model and the code using GFSSP, the user-subroutines can be shared with anyone who is a legal user of NASA’s code GFSSP.

References

Bandyopadhyay, A., and A. Majumdar. 2014. “Network flow simulation of fluid transients in rocket propulsion systems.” J. Propul. Power 30 (6): 1646–1653. https://doi.org/10.2514/1.B35194.
Lee, N. H. 2005. “Effect of pressurization and expulsion of entrapped air in pipelines.” Ph.D. thesis, Dept. of Civil and Environmental Engineering, Georgia Institute of Technology.
Lee, N. H., and C. S. Martin. 1999. “Experimental and analytical investigation of entrapped air in a horizontal pipe.” In Proc., 3rd ASME/JSME Joint Fluids Engineering Conf., 1–8. New York: ASME.
Majumdar, A. K., A. C. LeClair, R. Moore, and P. A. Schallhorn. 2013. Generalized fluid system simulation program, version 6.0. NASA/TM-2013-217492. Huntsville, AL: NASA Marshall Space Flight Center.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 34Issue 2March 2021

History

Received: May 30, 2018
Accepted: Oct 12, 2020
Published online: Jan 6, 2021
Published in print: Mar 1, 2021
Discussion open until: Jun 6, 2021

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Authors

Affiliations

Alak Bandyopadhyay [email protected]
Associate Professor, Computer Science, Alabama A&M Univ., Normal, AL 35762 (corresponding author). Email: [email protected]
Alok Majumdar [email protected]
Aerospace Technologist, Thermal Analysis Br, NASA Marshall Space Flight Center, Bldg. 4203, Martin Rd. Southwest, Huntsville, AL 35812. Email: [email protected]
Paul Schallhorn [email protected]
Branch Chief, NASA Launch Service, Mail Stop VAH30, Kennedy Space Ctr, FL 32899. Email: [email protected]

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