Evolutionary Algorithm Shape Optimization of a Hypersonic Flight Experiment Nose Cone, NR Deepak, T Ray, RR Boyce, Journal of Spacecraft and Rockets 45 (3), 428-237
Simulations of hypersonic, high-enthalpy separated flow over a'tick'configuration, JN Moss, S O'Byrne, NR Deepak, SL Gai, AIP Conference Proceedings 1501 (1), 1453-1460
High-enthalpy flow over a rearward-facing step–a computational study, NR Deepak, SL Gai, AJ Neely, Journal of fluid mechanics 695, 405-438
A Computational Investigation of Laminar Shock/Wave Boundary Layer Interactions, NR Deepak, SL Gai, AJ Neely, The Aeronautical Journal 117 (1187), 27-56
A computational study of high enthalpy flow over a rearward facing step, NR Deepak, SL Gai, AJ Neely, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, FL,
Aerothermodynamics of hypersonic shock wave boundary layer interactions, NR Deepak, SL Gai, AJ Neely, Proc. of 17th Australian Fluid Mechanics Conference
Hypersonic High-Enthalpy Flow in a Leading-edge Separation, NR Deepak, SL Gai, SO Byrne, JN Moss, 29th International Symposium on Shock Waves
Nose cone design optimization for a hypersonic flight experiment trajectory, NR Deepak, T Ray, R Boyce, 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference
Computational Studies of Hypersonic High Enthalpy Separated Flows, NR Deepak, PhD Thesis, University of New South Wales, Australian Defence Force Academy
Hypersonic Leading Edge Separation, A Khraibut, NR Deepak, SL Gai, AJ Neely, 19 Australasian Fluid Mechanics Conference, Melbourne, Australia
Investigation of Heat-Flux in High Enthalpy Hypersonic Flow Over a Rearward-Facing Step, NR Deepak, SL Gai, AJ Neely, International Journal of Hypersonics 1 (2), 115-134
Investigations of flow through the diffuser of IISc Hypersonic Wind Tunnel, NR Deepak, G Jagadeesh, B Vasudevan, 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference
Hypersonic High-Enthalpy Flow in a Leading-Edge Separation, NR Deepak, SL Gai, O Byrne S, M J.N, 29th International Symposium on Shock Waves 1. ISSW 2013 1, 521-526
A Numerical Study of High Enthalpy Flow over a Rearward Facing Step with Rounded Corners, NR Deepak, SL Gai, AJ Neely, 28th International Symposium on Shock Waves: Vol 2, 239-244
Experimental and numerical investigation of a hypersonic shock tunnel flow past a blunted cone, R Hruschka, G Park, N Deepak, SO Byrne, H Kleine, 27th International Symposium on Shock Waves
Laser-Induced-Fluorescence- Based Doppler Velocimetry of a Hypersonic Shock Tunnel Flow around a Model of a Planetary Entry Configuration, RB Hruschka, NR Deepak, G Park, SJO Byrne, HH Kleine, SL Gai, 5th Australian Conference on Laser Diagnostics in Fluid Mechanics and Combustion, 2008
Characterization of a Hypersonic Low-density Flow for Separated Flow Investigations, S O’Byrne, SL Gai, NR Deepak, Y Krishna, JN Moss