Technical Papers
Feb 22, 2024

Magnetohydrodynamic Control of a Hypersonic Shock–Turbulent Boundary Layer Interaction

Publication: Journal of Aerospace Engineering
Volume 37, Issue 3

Abstract

High-speed flows over a 34° compression corner subjected to several types of applied electromagnetic fields are numerically investigated. A coupled model for the turbulent flow field and the externally applied electromagnetic field is established based on the low magnetic Reynolds number assumption. The advection upstream splitting method with pressure-based weight function (AUSMPW) scheme and the lower upper symmetric Gauss Seidel (LUSGS) method are implemented to solve turbulent magnetohydrodynamic (MHD) flow equations. Numerical results demonstrate that the performance of MHD separation flow control is determined mainly by the Lorentz force in the turbulent boundary layer. For the counter-flow Lorentz force, the velocity fluid in the boundary layer can be retarded, and a significant temperature increase was observed. The decelerating Lorentz force significantly brings negative effects on the turbulent skin friction coefficients and increases the static pressure locally. Furthermore, the position of the MHD zone has a significant impact on the control efficiency of the ramp-induced separation. With an external electric and magnetic field applied, the low-velocity fluid in the boundary layer can be accelerated, and the Lorentz force directed along the stream can reduce the size of the separation bubble.

Get full access to this article

View all available purchase options and get full access to this article.

Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

This work was supported by the National Key Research and Development Plan of China (No. 2019YFA0405200).

References

Atkinson, M. D., J. Poggie, and J. A. Camberos. 2012. “Control of separated flow in a reflected shock interaction using a magnetically-accelerated surface discharge.” Phys. Fluids 24 (12): 126102. https://doi.org/10.1063/1.4772197.
Bobashev, S. V., N. P. Mende, and V. A. Sakharov. 2003. “MHD control of the separation phenomenon in a supersonic xenon plasma flow.” In Proc., AIAA Paper No. 2003-168. Reston, VA: American Institute of Aeronautics and Astronautics.
Dietiker, J. F., and K. A. Hoffmann. 2003. “Modified one-equation turbulence models for turbulent magnetohydrodynamic flows.” J. Thermophys. Heat Transfer 17 (4): 509–520. https://doi.org/10.2514/2.6796.
Elfstrom, G. M. 1972. “Turbulent hypersonic flow at a wedge-compression corner.” J. Fluid Mech. 53 (1): 113–127. https://doi.org/10.1017/S0022112072000060.
Fujino, T., and Y. Shimosawa. 2016. “Numerical study of magnetohydrodynamic flow control along superorbital reentry trajectories.” J. Spacecr. Rockets 53 (3): 528–537. https://doi.org/10.2514/1.A33340.
Gai, S., and A. Khraibu. 2019. “Hypersonic compression corner flow with large separated regions.” J. Fluid Mech. 877 (Aug): 471–494. https://doi.org/10.1017/jfm.2019.599.
Gatski, T. B., and G. Erlebacher. 2002. Numerical simulation of a spatially evolving supersonic turbulent boundary layer.. Hampton, VA: National Aeronautics and Space Administration.
Jiang, Z. J., and C. Yan. 2019. “On the use of thermally perfect gas model for heating prediction of laminar and turbulent STBLI.” Aerosp. Sci. Technol. 95 (Jun): 105484. https://doi.org/10.1016/j.ast.2019.105484.
Kalra, C. S., M. N. Shneider, and R. B. Miles. 2009. “Numerical study of boundary layer separation control using magnetogasdynamic plasma actuators.” Phys. Fluids 21 (10): 106101. https://doi.org/10.1063/1.3233658.
Khan, O. U., K. A. Hoffmann, and J. F. Dietiker. 2007. “Validity of low magnetic Reynolds number formulation of magnetofluiddynamic.” In Proc., AIAA Paper No. 2007-4374. Reston, VA: American Institute of Aeronautics and Astronautics.
Li, K., J. Liu, and W. Q. Liu. 2017. “Mechanism analysis of magnetohydrodynamic heat shield system and optimization of externally applied magnetic field.” Acta Astronaut. 133 (Jan): 14–23. https://doi.org/10.1016/j.actaastro.2016.12.036.
Li, K., and W. Q. Liu. 2016. “Analysis of the magnetohydrodynamic heat shield system for hypersonic vehicles.” [In Chinese.] Acta Phys. Sin. 65 (6) 064701. https://doi.org/10.7498/aps.65.064701.
Li, Y. W., Y. H. Li, and H. Y. Lu. 2011. “Preliminary experimental investigation on MHD Power generation using seeded supersonic argon flow as working fluid.” Chin. J. Aeronaut. 24 (6): 701–708. https://doi.org/10.1016/S1000-9361(11)60082-4.
Lu, H. Y., and D. Chao. 2015. “Three-dimensional design and numerical simulation of magnetohydrodynamic controlled hypersonic inlets.” Proc. IMechE Part G: J. Aerosp. Eng. 226 (G8): 20151002. https://doi.org/10.1177/0954410011416059.
Luo, S. C., J. Liu, and H. Jiang. 2020. “Grid convergence and influence of wall temperature in the calculation of thermochemical non-equilibrium heat flux.” J. Phys. D: Appl. Phys. 53 (28): 285502. https://doi.org/10.1088/1361-6463/ab813c.
Meyer, R., N. Chintala, and B. Bystrivky. 2004. “Lorentz force effect on supersonic ionized boundary layer.” In Proc., AIAA Paper No. 2004-510. Reston, VA: American Institute of Aeronautics and Astronautics.
Nagata, Y., K. Yamada, and T. Abe. 2013. “Hypersonic double-cone flow with applied magnetic field.” J. Spacecr. Rockets 50 (5): 981–991. https://doi.org/10.2514/1.A32351.
Pasha, A. A., and K. A. Juhany. 2020. “Numerical simulation of compression corner flows at Mach number 9.” Chin. J. Aeronaut. 33 (6): 1611–1624. https://doi.org/10.1016/j.cja.2020.01.005.
Pirozzoli, S., F. Grasso, and T. B. Gatski. 2004. “Direct numerical simulation and analysis of a spatially evolving supersonic turbulent boundary layer at M=2.25.” Phys. Fluids 16 (3): 530–545. https://doi.org/10.1063/1.1637604.
Qu, F., J. J. Chen, D. Sun, J. Q. Bai, and G. Zuo. 2019. “A grid strategy for predicting the space plane’s hypersonic aerodynamic heating loads.” Aerosp. Sci. Technol. 86 (Apr): 659–670. https://doi.org/10.1016/j.ast.2019.01.049.
Saito, S., K. Udgawa, and K. Kawaguchi. 2008. “Boundary layer separation control by MHD interaction.” In Proc., AIAA Paper No. 2008-1091. Reston, VA: American Institute of Aeronautics and Astronautics.
Shang, J. S., S. T. Surzhikovb, R. Kimmelc, and D. Gaitondec. 2002. “Mechanisms of plasma actuators for hypersonic flow control.” Prog. Aerosp. Sci. 41 (Sep): 642–668.
Updike, G. A., J. S. Shang, and D. V. Gaitonde. 2005. “Hypersonic separated flow control using magneto-aerodynamic interaction.” In Proc., AIAA Paper No. 2005-164. Reston, VA: American Institute of Aeronautics and Astronautics.
Van, D. M., and A. Nedungadi. 2004. “Plasma aerodynamic flow control for hypersonic inlets.” In Proc., AIAA Paper No. 2004-4129. Reston, VA: American Institute of Aeronautics and Astronautics.
Wang, T. 2007. “Computational simulations of supersonic magnetohydrodynamic flow control.” Ph.D. dissertation, Faculty of the Graduate School, Univ. of Minnesota.
Zaidi, S. H., T. Smith, and S. Macheret. 2006. “Snowplow surface discharge in magnetic field for high speed boundary layer control.” In Proc., AIAA Paper No. 2006-1006. Reston, VA: American Institute of Aeronautics and Astronautics.

Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 3May 2024

History

Received: Sep 7, 2022
Accepted: Dec 6, 2023
Published online: Feb 22, 2024
Published in print: May 1, 2024
Discussion open until: Jul 22, 2024

Permissions

Request permissions for this article.

ASCE Technical Topics:

Authors

Affiliations

Shichao Luo [email protected]
Ph.D. Research Scholar, Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China (corresponding author). Email: [email protected]
Professor, Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China. Email: [email protected]
Professor, Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China. Email: [email protected]

Metrics & Citations

Metrics

Citations

Download citation

If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.

View Options

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Media

Figures

Other

Tables

Share

Share

Copy the content Link

Share with email

Email a colleague

Share