Faculty
Aqib Khan
DST INSPIRE Fellow

Mobile: +91 70541 32609
Telephone: +91-80-2293-2317
E-mail: aqibkhan at iisc.ac.in
kaqib111@gmail.com

New opening-Research Associate/Assistant position-July 2024.




Education

- PhD and M-Tech (Integrated), Indian Institute of Technology, IIT Kanpur, India. from 2015-2022.
(Major: Aerospace Engineering)
- Bachelor of Technology, Aligarh Muslim University, AMU-Aligarh, India from 2011-2015.
(Major: Mechanical Engineering)
- Diploma in Engineering, Aligarh Muslim University, AMU-Aligarh, India from 2008-2011.
(Major: Plastic Technology)

Courses

Tutor: Engineering Graphics
Experiments in Aerospace Engineering.

Research

- Shock waves and instabilities in granular flows.
An experimental campaign is launched at the Aerospace Engineering department to investigate shock waves and instabilities in granular flows under the guidance of Prof. Sanjay Kumar and Prof. Rakesh Kumar. The project is funded by the Department of Science and Engineering Board, India.
- Swept shock wave/turbulent boundary layer interaction.
An experimental investigation is carried out to control the steady and unsteady characteristics of the threedimensional swept shock wave and turbulent boundary layer interaction using micro-vortex generators for applications in supersonic inlets. Research work is conducted in collaboration with National Aerospace Laboratories (NAL), Bangalore, India.
- Experimental and numerical investigation of plug nozzle flows.
The project involves the development of plug nozzles for application to launch vehicles. The project is supervised by Dr. Rakesh Kumar and is funded by the Indian Space Research Organization (ISRO),India.
- Aerodynamic and aeroacoustic investigation of multiple jets.
The project involves the investigation and control of the mixing characteristics of supersonic jets from converging-diverging nozzles operating under chocked conditions. Vortex generators are used to enhance the mixing characteristics and reduce the screech and shock-associated noise from closely spaced twin jets. The project is supervised by Dr. Rakesh Kumar.
- Supersonic jet control using fluidic injection.
The aerodynamic and aeroacoustic characteristics of a supersonic jet exiting from a converging-diverging nozzle are manipulated by injecting secondary jets from mini injectors that are oriented normal to the primary jet. The project is supervised by Dr. Rakesh Kumar and Dr. Arun Kumar Perumal
 

Awards & Honors

1) INSPIRE Faculty Fellowship awarded by the Department of Science and Technology in the year 2024.
2) Institute of Eminence Postdoctoral Fellowship awarded by the Indian Institute of Science Bangalore in the year 2024.
3) Kumar-Gandhi award for the best talk at the Chemical Engineering Symposium at IISc held on 15 - 16th December 2023.
4) Article (Khan et al. 2020, https://doi.org/10.1017/jfm.2019.988) is selected as a featured article for extended review and discussion by an acknowledged and invited expert in the field. The review article based on this work is published in Focus on Fluids section of the Journal of Fluid Mechanics explaining the context, importance and implications of the underlying paper to a wider scientific audience, highlighting both the key findings and breakthroughs of the paper and the implications of the research for future activity. Johnson, Chris G. ”Shocking granular flows.” Journal of Fluid Mechanics 890 (2020).DOI: https://doi.org/10.1017/jfm.2020.61
5) Distinguished Student Award on behalf of the APS Forum on International Physics (FIP) at the 2022 APS March Meeting.
6) Best Poster Award, CompFlu, December 2022, IIT Kharagpur
7) International Travel Support from the Department of Science and Technology to give a talk at the AIAA Aviation Forum held in Dallas, Texas in the USA in 2019.
8) First position in Diploma in Engineering (class of 2011).

Publications

Publications:

1) Khan, A., Chidambaranathan, M., Verma, S.B. et al. Swept shock/boundary-layer interaction control using micro-vortex generators. Shock Waves 33, 553-567 (2024). DOI: https://doi.org/10. 1007/s00193-023-01155-0
2) Jaiswal, Y., Khan, A., Kumar, R., and Kumar, S."Shocked confined-granular flow over obstacles". Journal of Fluid Mechanics, 960, A21, (2023). DOI: https://doi.org/10.1017/jfm.2023. 211
3) Khan, A., Hankare, P., Verma, S., Jaiswal, Y., Kumar, R., and Kumar, S. "Detachment of strong shocks in confined granular flows". Journal of Fluid Mechanics, 935, A13, (2022). DOI: https://doi:10.1017/jfm.2022.5
4) Mathews, A. K., Khan, A., Sharma, B., Kumar, S., and Kumar, R., "A numerical investigation of granular shock waves over a circular cylinder using the discrete element method",Journal of Fluid Mechanics, 936, A13, (2022). DOI: https://doi:10.1017/jfm.2022.62
5) Khan, A., Verma, S., Hankare, P., Kumar, R., and Kumar, S., "Shock-shock interactions in granular flows", Journal of Fluid Mechanics 884 R4, (2020). DOI: https://doi.org/10.1017/jfm.2019.988
6) Khan, A., Nageswara Rao, A., Baghel, T., Perumal, A. K., and Kumar, R. "Parametric study and scaling of Mach 1.5 jet manipulation using steady fluidic injection", Physics of Fluids, (2022) 34(3), 036107. DOI: https://doi.org/10.1063/5.0078089
7) Pragya Patel, Ramdas Tiwari, Aqib Khan, Shivam Verma, Rakesh Kumar and Sanjay Kumar, "Shock profiles and wake structures in granular flow past obstacles", Journal of Flow Visualization and Image Processing. DOI: https://10.1615/JFlowVisImageProc.2022040664
8) Faheem, M., Khan, A., Kumar, R., Khan, Sher A. Asrar, W. and Sapardi, Azan M., "Experimental investigation of the effect of cross wire on the flow field of elliptic jet." International Journal of Heat and Fluid Flow, 90 (2021): p.108834. DOI: https://doi.org/10.1016/j.ijheatfluidflow.2021.108834
9) Khan, A., A. S. Bhesania, and R. Kumar., "An experimental study on the control of plug nozzle jets." Shock Waves (2021): 1-17. DOI: https://doi.org/10.1007/s00193-021-00989-w
10) Faheem, M., Khan, A., Kumar, R., Khan, Sher A. Asrar, W. and Sapardi, Azan M., "Experimental study on the mean flow characteristics of a supersonic multiple jet configuration". Aerospace Science and Technology, 108 (2021): 106377. DOI: https://doi.org/10.1016/j.ast.2020.106377
11) Chaudhary M, Krishna TV, Nanda SR, Karthick SK, Khan A, De A, Sugarno IM., "On the fluidic behavior of an over-expanded planar plug nozzle under lateral confinement". Physics of Fluids (2020);32(8):086106. DOI: https://doi.org/10.1063/5.0015885
12) Panthi, R., Krishna, T. V., Nanda, S. R., Khan, A., Kumar, R., and Sugarno, M. I., "Experimental Study of Impinging Plug Nozzle Jet Using a Vortex Generator". Journal of Spacecraft and Rockets, 57, no. 6 (2020): 1414-1418. DOI: https://doi.org/10.2514/1.A34760
13) Khan, A., Akram, S., and Kumar, R., "Experimental study on enhancement of supersonic twin-jet mixing by vortex generators." Aerospace Science and Technology (2019): 105521. DOI: https://doi.org/10.1016/j.ast.2019.105521
14) Khan, A., Panthi, R., Kumar, R., and Ibrahim, S. M., "Experimental investigation of the effect of extended cowl on the flow field of planar plug nozzles". Aerospace Science and Technology, Vol. 88, (2019), pp. 208-221. DOI: https://doi.org/10.1016/j.ast.2019.03.011
15) Khan, A., Kumar, R., Verma, S. B., and Manisankar, C., "Effect of cross wire tab orientation on twin jet mixing characteristics." Experimental Thermal and Fluid Science 99 (2018): 344-356. DOI: https://doi.org/10.1016/j.expthermflusci.2018.08.005
16) Khan, A., and Kumar, R., "Experimental study and passive control of overexpanded plug nozzle jet". Journal of Spacecraft and Rockets 55, no. 3 (2017): 778-782. DOI: https://doi.org/10.2514/1.A34039