Brian Joseph Cantwell, Ph.D.
Affiliations: | Stanford University, Palo Alto, CA |
Area:
turbulenceGoogle:
"Brian Cantwell"Bio:
Cantwell, Brian Joseph (1976) A flying hot wire study of the turbulent near wake of a circular cylinder at a Reynolds number of 140,000. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/QKGW-CA84.
Parents
Sign in to add mentorDonald Earl Coles | grad student | 1976 | Caltech | |
(A flying hot wire study of the turbulent near wake of a circular cylinder at a Reynolds number of 140,000) |
Children
Sign in to add traineeGary Arthur Allen, Jr. | grad student | 1984 | Stanford |
Jacqueline H. Chen | grad student | 1989 | Stanford |
Owen Clayton Brown | grad student | 2000 | Stanford |
Patrick John Moriarty | grad student | 2000 | Stanford |
Paul Castellucci | grad student | 2007 | Stanford |
William G. Hart | grad student | 2007 | Stanford |
Siina Ilona Haapanen | grad student | 2008 | Stanford |
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Publications
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Jens ET, Karp AC, Miller VA, et al. (2020) Experimental Visualization of Hybrid Combustion: Results at Elevated Pressures Journal of Propulsion and Power. 36: 33-46 |
Cantwell BJ. (2019) A universal velocity profile for smooth wall pipe flow Journal of Fluid Mechanics. 878: 834-874 |
Coates AM, Mathias DL, Cantwell BJ. (2019) Numerical investigation of the effect of obstacle shape on deflagration to detonation transition in a hydrogen–air mixture Combustion and Flame. 209: 278-290 |
Jens ET, Miller VA, Cantwell BJ. (2016) Schlieren and OH* chemiluminescence imaging of combustion in a turbulent boundary layer over a solid fuel Experiments in Fluids. 57 |
Cantwell BJ. (2014) Similarity solution of fuel mass transfer, port mass flux coupling in hybrid propulsion Journal of Engineering Mathematics. 84: 19-40 |
Chandler AA, Cantwell BJ, Scott Hubbard G, et al. (2011) Feasibility of a single port Hybrid Propulsion system for a Mars Ascent Vehicle Acta Astronautica. 69: 1066-1072 |
Karabeyoglu MA, Cantwell BJ, Zilliac G. (2007) Development of scalable space-time averaged regression rate expressions for hybrid rockets Journal of Propulsion and Power. 23: 737-747 |
Arif Karabeyoglu M, De Zilwa S, Cantwell B, et al. (2005) Modeling of hybrid rocket low frequency instabilities Journal of Propulsion and Power. 21: 1107-1116 |
Karabeyoglu A, Zilliac G, Cantwell BJ, et al. (2004) Scale-up tests of high regression rate paraffin-based hybrid rocket fuels Journal of Propulsion and Power. 20: 1037-1045 |
Cantwell B. (2004) A singularity-free model of the local velocity gradient and acceleration gradient structure of turbulent flow Fluid Mechanics and Its Applications. 71: 247-260 |