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  1. Multi-Point Design Optimization of Busemann Based Intakes for Scramjet-Powered Ascent Flight via Surrogate-Assisted Evolutionary Algorithms

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

    Hideaki Ogawa, Shuvayan Brahmachary

  2. Comment on “A new approach for the design of hypersonic scramjet inlets” [Phys. Fluids 24, 086103 (2012)]

    Article • Physics of Fluids, July 2020, American Institute of Physics

    Shuvayan Brahmachary