Now showing items 1-2 of 2

    • Dynamic Mode Decomposition Of Detonation Waves 

      Kumar, Rahul (Aerospace Engineering, 2012-07-25)
      Dynamic mode decomposition is applied to study the self-excited fluctuations supported by transversely unstable detonations. The focus of this study is on the effect of forcing on the limit cycle solutions. Using DMD, only ...
    • Pulsed Detonation Engine Nozzle Design and Analysis 

      Kumar, Rahul; 0000-0002-2991-7192 (2019-12-04)
      For a hypersonic flight mission, different flight regimes have been recognized. The successful and efficient operation of the aircraft to traverse through all the flight regimes requires the integration of various propulsion ...