Mr Sudip Bhattrai

PhD Candidate, UNSW Canberra Hypersonics
School of Engineering and Information Technology

LOCATION

Building 20, G03

  • ABOUT
  • PUBLICATIONS

PhD Candidate, Aerospace Engineering, UNSW Canberra Hypersonics (S2, 2017 - S1, 2021)

Supervisor: Professor Andrew J Neely

Research supported by US Air Force Office of Scientific Research: 

  • Unit Cases to Investigate Hypersonic Fluid-Structure Interactions / USAF AFOSR FA2386-19-1-4027. 
  • Characterisation and control of a flap undergoing hypersonic fluid-structure interaction / USAF AFOSR FA2386-16-1-4024
 

Journal articles

Paudel S; Bhattarai S; Bhattrai S; Bomjan B, 2019, 'Effects of magnetohydrodynamics on temperature and shock standoff distance in a supersonic flow over a blunt body', Progress in Computational Fluid Dynamics, vol. 19, pp. 264 - 271, http://dx.doi.org/10.1504/PCFD.2019.100876

Bomjan B; Bhattrai S; Tang H, 2018, 'Characterization of induction and transition methods of oblique detonation waves over dual-angle wedge', Aerospace Science and Technology, vol. 82-83, pp. 394 - 401, http://dx.doi.org/10.1016/j.ast.2018.07.038

Bhattrai S; de Baar JHS; Neely AJ, 2018, 'Efficient uncertainty quantification for a hypersonic trailing-edge flap, using gradient-enhanced kriging', Aerospace Science and Technology, vol. 80, pp. 261 - 268, http://dx.doi.org/10.1016/j.ast.2018.06.036

Chen N; Esfehani SA; Bhattrai S; Liu Y; Tang H, 2018, 'Numerical Study on Effects of Equivalence Ratio on Initiation Characteristics of Oblique Detonation Waves', Tuijin Jishu/Journal of Propulsion Technology, vol. 39, pp. 2798 - 2805, http://dx.doi.org/10.13675/j.cnki.tjjs.2018.12.019

Chen N; Bhattrai S; Tang H, 2018, 'Numerical simulation of influence of temperature disturbance on oblique detonation wave structure', Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, vol. 44, pp. 1537 - 1546, http://dx.doi.org/10.13700/j.bh.1001-5965.2017.0561

Bhattrai S; Tang H, 2017, 'Formation of near-Chapman–Jouguet oblique detonation wave over a dual-angle ramp', Aerospace Science and Technology, vol. 63, pp. 1 - 8, http://dx.doi.org/10.1016/j.ast.2016.12.010

Bhattrai S; Tang H, 2013, 'Comparative performance analysis of combined-cycle pulse detonation turbofan engines (PDTEs)', Propulsion and Power Research, vol. 2, pp. 214 - 224, http://dx.doi.org/10.1016/j.jppr.2013.04.007

Zhang C; Tang H; Li M; Bhattrai S, 2012, 'Effects of equivalence ratio and gap size on the propagation behavior of detonations', Hangkong Dongli Xuebao/Journal of Aerospace Power, vol. 27, pp. 1948 - 1957

Conference Papers

Bhattrai S; McQuellin LP; Currao GMD; Neely AJ; Buttsworth DR, 2020, 'Experimental study of the aeroelastic response and performance of a hypersonic intake', in 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2020

Bhattrai S; McQuellin LP; Currao G; Neely AJ; Buttsworth DR, 2018, 'Influence of hypersonic fluid-structure interaction on the control authority of a trailing-edge flap', in 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, Orlando, FL, presented at 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, Orlando, FL, 17 September 2018 - 19 September 2018, http://dx.doi.org/10.2514/6.2018-5265

Bhattrai S; Neely AJ; Currao GMD; McQuellin LP, 2018, 'The effect of streamwise pressure distribution on the aeroelastic deformation of hypersonic trailing-edge flaps', in Proceedings of the 21st Australasian Fluid Mechanics Conference, AFMC 2018

Bhattrai S; Neely AJ; Currao GMD; McQuellin LP, 2018, 'The effect of streamwise pressure distribution on the aeroelastic deformation of hypersonic trailing-edge flaps', in Proceedings of the 21st Australasian Fluid Mechanics Conference, AFMC 2018

Bhattarai S; Poudel KR; Bhatta N; Mahat S; Bhattrai S; Thapa Magar KS, 2018, 'Modeling and development of baseline guidance navigation and control system for medical delivery UAV', in AIAA Information Systems-AIAA Infotech at Aerospace, 2018, http://dx.doi.org/10.2514/6.2018-0508