Ashish Singh

Ashish Singh

I am a Post-doctoral research associate at the department of Aerospace & Mechanical Engineering (AME) at the Univeristy of Arizona. My primary research work focuses on:

  1. How structural motion of airfoils caused by unsteady loading affects transition from laminar to turbulent flow at low flight Reynolds numbers
  2. Understanding hypersonic transition in the presence of shock boundary layer interaction
I study subsonic transition physics through flight testing (on an instrumented scaled model X-56 aircraft) and using experimental methods such as Particle Image Velocimetry (PIV), Schlieren flow visualization, hot wire anemometry, pressure measurements etc in a large (3 ft x 4 ft x 12 ft) subsonic wind tunnel. My reserach on hypersonic tansition is done in a Mach 5 Ludwig tube (at Reynolds number of upto 20 million per meter) facility and an in-draft supersonic tunnel. I employ high frequency pressure transducers and high-speed imagining techniques. I'm also interested in using Linear Stability Theory (LST) and Computational Fluid Dynamics (CFD) to complement my experimental work.

Education

Doctor of Philosophy (PhD) - Aerospace Engineering at Univeristy of Arizona (2020)

Master of Science in Engineering (MSE) - Aerospace Engineering at University of Michigan Ann Arbor (2013)

Bachelor of Engineering (BE) - Visvesvarya Technological University (2010)