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  1. Volumetric Characterization of Experimental Flowfield in a Double-Fin SBLI at Mach 3

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    serdar seckin

  2. A Momentum Potential Theory-Based Framework for Analyzing Experimental Pressure-Sensitive Paint Data

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Anshul Suri, serdar seckin

  3. Analysis of Noise Reduction in Dual Impinging Jets with Microjets

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Naveen Rohilla, serdar seckin

  4. Fluid-Structure Interaction Insights From Pressure-Sensitive Paint Measurements for Double-Fin SBLI

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    serdar seckin, Anshul Suri

  5. Surface Properties of Double-Fin Generated Shock-Wave/Boundary-Layer Interactions

    Article • AIAA Journal, December 2023, American Institute of Aeronautics and Astronautics (AIAA)

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  6. Mapping 3D Acoustics of a Supersonic Diamond Jet: An Odyssey in the Golden Age of Aeroacoustics

    Article • June 2023, American Institute of Aeronautics and Astronautics (AIAA)

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  7. Three-Dimensional Flow Characterization of Double-Fin SBLI

    Article • June 2023, American Institute of Aeronautics and Astronautics (AIAA)

    serdar seckin

  8. Optimization of Microjet Control for Supersonic Impinging Jet Using Genetic Algorithm

    Article • June 2023, American Institute of Aeronautics and Astronautics (AIAA)

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  9. Mapping 3D Acoustics of a Supersonic Diamond Jet: An Odyssey in the Golden Age of Aeroacoustics

    Article • June 2023, American Institute of Aeronautics and Astronautics (AIAA)

    serdar seckin

  10. Three-Dimensional Flow Characterization of Double-Fin SBLI

    Article • June 2023, American Institute of Aeronautics and Astronautics (AIAA)

    serdar seckin

  11. Optimization of Microjet Control for Supersonic Impinging Jet Using Genetic Algorithm

    Article • June 2023, American Institute of Aeronautics and Astronautics (AIAA)

    serdar seckin

  12. A continuously scanning spatiotemporal averaging method for obtaining volumetric mean flow measurements with stereoscopic PIV

    Article • Experiments in Fluids, February 2023, Springer Science + Business Media

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  13. Dynamics and Response to Control of Single and Dual Supersonic Impinging Jets

    Article • AIAA Journal, May 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Vikas N. Bhargav, serdar seckin

  14. Dynamics and Response to Microjet Control of Dual Supersonic Impinging Jets

    Article • January 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Vikas N. Bhargav, serdar seckin

  15. Dynamics and Response to Microjet Control of Dual Supersonic Impinging Jets

    Article • January 2022, American Institute of Aeronautics and Astronautics (AIAA)

    serdar seckin

  16. Surface Properties of Double-Fin Generated Shock-Wave/Boundary-Layer Interactions

    Article • January 2022, American Institute of Aeronautics and Astronautics (AIAA)

    serdar seckin

  17. Surface Properties of Double-Fin Generated Shock-Wave/Boundary-Layer Interactions

    Article • January 2022, American Institute of Aeronautics and Astronautics (AIAA)

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  18. Active Flow Control of Single and Dual Supersonic Impinging Jets using Microjets

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Rajan Kumar, Dr Prabu Sellappan, Vikas N. Bhargav, serdar seckin

  19. Experimental study of the mean structure and quasi-conical scaling of a swept-compression-ramp interaction at Mach 2

    Article • Journal of Fluid Mechanics, February 2018, Cambridge University Press

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  20. POD Analysis of Unsteadiness Mechanisms within a Swept Compression-Ramp Shock-Wave Boundary-Layer Interaction at Mach 2

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

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  21. Role of Boundary-Layer on Unsteadiness on a Mach 2 Swept-Ramp Shock/Boundary-Layer Interaction Using 50 kHz PIV

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

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  22. Investigation of Unsteadiness in a Mach 2 Swept-Ramp Shock/Boundary-Layer Interaction Using 50 kHz PIV

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

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  23. Effect of Upstream Boundary Layer on Unsteadiness of Swept-Ramp Shock/Boundary Layer Interactions at Mach 2

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

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  24. Experimental Investigation of Unsteadiness of Swept-Ramp Shock/Boundary Layer Interactions at Mach 2

    Article • June 2015, American Institute of Aeronautics and Astronautics (AIAA)

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