Manoj Kumar K. Devaraj

Design of Optimized Two-Dimensional Scramjet Nozzle Contour for Hypersonic Vehicle Using Evolutionary Algorithms

Yogendra Singh, S. N. Omkar, Gopalan Jagadeesh, 2017 .

Experimental investigation of unstart dynamics driven by subsonic spillage in a hypersonic scramjet intake at Mach 6

Manoj Kumar K. Devaraj, G. Jagadeesh, Srisha M. V. Rao, 2020 .

Length scale for the estimation of buzz frequency in the limit of high mechanical blockage in mixed-compression intakes

Manoj Kumar K. Devaraj, G. Jagadeesh, Srisha M. V. Rao, 2021, Journal of Fluid Mechanics.

Investigation of local unstart in a hypersonic scramjet intake at a Mach number of 6

Manoj Kumar K. Devaraj, G. Jagadeesh, Srisha M. V. Rao, 2021 .

Limitations of Two-Shock Mixed Compression Intakes at Hypersonic Mach Numbers

Manoj Kumar K. Devaraj, G. Jagadeesh, Arjun J. Vedam, 2019, AIAA Aviation 2019 Forum.