Author

Akshay Prakash

Institution: Indian Institute of Technology Kharagpur

Observed institutions: Indian Institute of Technology Kharagpur, University of California, Los Angeles, University of California System

OpenAlex ID: A5105974198

High-Order Shock-Fitting Methods for Hypersonic Flow with Chemical and Thermal Nonequilibrium

2010 · Akshay Prakash, Neal Parsons, et al. · AIAA Fluid Dynamics Conference and Exhibit · 4

Floquet Analysis of Second Mode Disturbance in Hypersonic Boundary Layer with Wall Blowing

2022 · Chandan Kumar, Akshay Prakash · AIAA SciTech Forum · 2

Numerical Simulation of Planetary Reentry Aeroheating Over Blunt Bodies with Non-Equilibrium Reacting Flow and Surface Reactions

2009 · Akshay Prakash, Xiaolin Zhong · AIAA Aerospace Sciences Meeting · 2

Optimization of Blunt Nose Semi-spherical Heat-Shield in Hypersonic Flow at Mach 7.99

2022 · Chandan Kumar, Akshay Prakash · Lecture notes in mechanical engineering · 1

Numerical Simulation of Planetary Reentry Aeroheating Over Blunt Bodies with Non-equilibrium Reacting Flow

2008 · Akshay Prakash, Xiaolin Zhong · AIAA Aerospace Sciences Meeting and Exhibit · 1

Numerical Simulation of Receptivity to Freestream Acoustic Disturbances for Hypersonic Boundary Layer over a Blunt Body with Chemical and Thermal Nonequilibrium

2011 · Akshay Prakash · PhDT

Works count: 6

Citation count: 10

H-index: 2

I10-index: