Numerical Investigation of the Hypersonic Inlet under Throttling with Heat Source

Nurfathin Zahrolayali; Mohd Rashdan Saad; Azam Che Idris; Mohd Rosdzimin Abdul Rahman

doi:10.37934/cfdl.14.10.7986

Authors

Nurfathin Zahrolayali Department of Mechanical Engineering, Faculty of Engineering, Universiti Pertahanan Nasional Malaysia, Kem Sg. Besi, Kuala Lumpur, Malaysia
Mohd Rashdan Saad Department of Mechanical Engineering, Faculty of Engineering, Universiti Pertahanan Nasional Malaysia, Kem Sg. Besi, Kuala Lumpur, Malaysia
Azam Che Idris Faculty of Integrated Technologies, Universiti Brunei Darussalam, Brunei
Mohd Rosdzimin Abdul Rahman Department of Mechanical Engineering, Faculty of Engineering, Universiti Pertahanan Nasional Malaysia, Kem Sg. Besi, Kuala Lumpur, Malaysia

DOI:

https://doi.org/10.37934/cfdl.14.10.7986

Keywords:

Numerical Simulation, Hypersonic, Shock Wave Boundary Layer, Heat Source, Active Flow Control

Abstract

The influence of using a heat source to manage the shock wave boundary layer interactions (SWBLI) at the hypersonic inlet under throttling were studied numerically. This hypersonic inlet was created for a fluid flow Mach number of 5. The throttling was induced by a plug placed near the intake isolator's outlet. The study's parameters included the heat source power and size. The intake performance indicators were the total pressure recovery and the flow distortion. The position of the heat source was determined by studying the interplay of the shock waves from the compression ramp. The results demonstrated the existence of the shock waves at the heat source, and its influences on the SWBLI inside the isolator. This behaviour, led to an increase in the total pressure recovery and reduction of the flow distortion.

Downloads

Download data is not yet available.

Author Biography

Mohd Rosdzimin Abdul Rahman, Department of Mechanical Engineering, Faculty of Engineering, Universiti Pertahanan Nasional Malaysia, Kem Sg. Besi, Kuala Lumpur, Malaysia

rosdzimin@gmail.com

References

Delery, Jean M. "Shock wave/turbulent boundary layer interaction and its control." Progress in Aerospace Sciences 22, no. 4 (1985): 209-280. https://doi.org/10.1016/0376-0421(85)90001-6

Andersson, Niklas, Lars-Erik Eriksson, and Lars Davidson. "Large-eddy simulation of a Mach 0.75 jet." In 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, p. 3312. 2003. https://doi.org/10.2514/6.2003-3312

Dolling, David S. "Fifty years of shock-wave/boundary-layer interaction research: what next?." AIAA journal 39, no. 8 (2001): 1517-1531. https://doi.org/10.2514/2.1476

Krishnan, L., N. D. Sandham, and Johan Steelant. "Shock-wave/boundary-layer interactions in a model scramjet intake." AIAA journal 47, no. 7 (2009): 1680-1691. https://doi.org/10.2514/1.41107

Xie, Wen-Zhong, Zhong-Ming Wu, An-Yuan Yu, and Shengmin Guo. "Control of severe shock-wave/boundary-layer interactions in hypersonic inlets."Journal of Propulsion and Power34, no. 3 (2018): 614-623. https://doi.org/10.2514/1.B36614

Huang, Wei, Han Wu, Yan-guang Yang, Li Yan, and Shi-bin Li. "Recent advances in the shock wave/boundary layer interaction and its control in internal and external flows."Acta Astronautica174 (2020): 103-122. https://doi.org/10.1016/j.actaastro.2020.05.001

Jiang, Hao, Jun Liu, Shi-chao Luo, Jun-yuan Wang, and Wei Huang. "Hypersonic flow control of shock wave/turbulent boundary layer interactions using magnetohydrodynamic plasma actuators." Journal of Zhejiang University-SCIENCE A 21, no. 9 (2020): 745-760. https://doi.org/10.1631/jzus.A2000025

Hongyu, W. A. N. G., L. I. Jun, J. I. N. Di, D. A. I. Hui, G. A. N. Tian, and W. U. Yun. "Effect of a transverse plasma jet on a shock wave induced by a ramp."Chinese journal of Aeronautics30, no. 6 (2017): 1854-1865. https://doi.org/10.1016/j.cja.2017.09.004

Mengxiao, Tang, Wu Yun, Wang Hongyu, Guo Shanguang, Sun Zhengzhong, and Sheng Jiaming. "Characterization of transverse plasma jet and its effects on ramp induced separation." Experimental Thermal and Fluid Science 99 (2018): 584-594. https://doi.org/10.1016/j.expthermflusci.2018.05.023

Macheret, Sergey O., Mikhail N. Shneider, and Richard B. Miles. "Scramjet inlet control by off-body energy addition: a virtual cowl." AIAA journal 42, no. 11 (2004): 2294-2302. https://doi.org/10.2514/1.3997

Kremeyer, Kevin, Kurt Sebastian, and Chi-Wang Shu. "Computational study of shock mitigation and drag reduction by pulsed energy lines." AIAA journal 44, no. 8 (2006): 1720-1731. https://doi.org/10.2514/1.17854

Russell, A., M. Myokan, H. Bottini, A. Sasoh, H. Zare-Behtash, and K. Kontis. "Application of laser energy deposition

Pham, Hoang Son, Tatsuro Shoda, Takahiro Tamba, Akira Iwakawa, and Akihiro Sasoh. "Impacts of laser energy deposition on flow instability over double-cone model."AIAA Journal55, no. 9 (2017): 2992-3000. https://doi.org/10.2514/1.J055670

Watanabe, Yasumasa, Alec Houpt, and Sergey B. Leonov. "Plasma-assisted control of supersonic flow over a compression ramp." Aerospace 6, no. 3 (2019): 35. https://doi.org/10.3390/aerospace6030035

Feng, Xie, Li Jie, and Yao Cheng. "Study on control of hypersonic aerodynamic force by quasi-DC discharge plasma energy deposition." Acta Astronautica 187 (2021): 325-334. https://doi.org/10.1016/J.ACTAASTRO.2021.06.049

Dahalan, Md Nizam, Ahmad Fitri Suni, Iskandar Shah Ishak, Nik Ahmad Ridhwan Nik Mohd, and Shabudin Mat. "Aerodynamic study of air flow over a curved fin rocket." Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 40, no. 1 (2017): 46-58.

Hussein, Emad Qasem, Farhan Lafta Rashid, and Haider Nadhom Azziz. "Aerodynamic heating distribution for temperature prediction of fast flying body nose using CFD." Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 64, no. 2 (2019): 183-195.

Idris, Azam Che, Mohd Rashdan Saad, and Konstantinos Kontis. "Potential of Micro-Vortex Generators in Enhancing the Quality of Flow in a Hypersonic Inlet-Isolator." Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 77, no. 1 (2021): 1-10. https://doi.org/10.37934/arfmts.77.1.110

Alekseyenko, Serhii, Andrii Dreus, Mykola Dron, and Olexandr Brazaluk. "Numerical Study of Aerodynamic Characteristics of a Pointed Plate of Variable Elongation in Subsonic and Supersonic Gas Flow." Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 96, no. 2 (2022): 88-97. https://doi.org/10.37934/arfmts.96.2.8897

Alberti, Andrea, Alessandro Munafò, Carlos Pantano, and Marco Panesi. "Supersonic and hypersonic non- equilibrium flow control using laser energy deposition." In AIAA Aviation 2019 Forum, p. 2867. 2019. https://doi.org/10.2514/6.2019-2867

Idris, Azam Che, Mohd Rashdan Saad, Hossein Zare-Behtash, and Konstantinos Kontis. "Luminescent measurement systems for the investigation of a scramjet inlet-isolator."Sensors14, no. 4 (2014): 6606-6632. https://doi.org/10.3390/s140406606

Li, Zhufei, Wenzhi Gao, Hongliang Jiang, and Jiming Yang. "Unsteady behaviors of a hypersonic inlet caused by throttling in shock tunnel." AIAA journal 51, no. 10 (2013): 2485-2492. https://doi.org/10.2514/1.J052384

Sun, Pei-Zhao, Hai-Tao Shi, and Xi-Yun Lu. "Numerical investigation of the unsteady behavior of a hypersonic inlet under throttling." Procedia Engineering 126 (2015): 179-183. https://doi.org/10.1016/j.proeng.2015.11.210

Devaraj, Manoj Kumar K., Prahallada Jutur, Srisha MV Rao, Gopalan Jagadeesh, and Ganesh TK Anavardham.

"Experimental investigation of unstart dynamics driven by subsonic spillage in a hypersonic scramjet intake at Mach

" Physics of Fluids 32, no. 2 (2020): 026103. https://doi.org/10.1063/1.5135096

Sepahi-Younsi, Javad, and Safa Esmaeili. "Performance enhancement of a supersonic air intake by applying a heat

source." Journal of Aerospace Engineering 33, no. 5 (2020): 04020048. https://doi.org/10.1061/(ASCE)AS.1943-

0001170

Gudmundsson, Snorri. General aviation aircraft design: Applied Methods and Procedures. Butterworth-Heinemann, 2013. https://doi.org/10.1016/C2011-0-06824-2