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Andrews, D. R. (author), Bourne, N. K. (author), Brown, E. N. (author), Dear, J. P. (author), Dickson, P. (author), Freeman, C. J. (author), Goveas, S. G. (author), Hauser, H. (author), van der Zwaag, S. (author)Professor John Edwin Field passed away on October 21st, 2020 at the age of 84. Professor Field was widely regarded as a leader in high-strain rate physics and explosives. During his career in the Physics and Chemistry of Solids (PCS) Group of the Cavendish Laboratory at Cambridge University, John made major contributions into our...review 2021
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- Andrews, D.J. (author), Duchateau, E.A.E. (author), Gillespe, J.W. (author), Hopman, J.J. (author), Pawling, R.G. (author), Singer, D.J. (author) conference paper 2012
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- Andrews, David J. (author) report 2008
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- Andrews, David J. (author) report 2008
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- Andrews, G.S. (author), Bosch, M.A. (author), Nederlof, C. (author), Nieuwstraten, R. (author), Stemmer, R. (author) report 2006
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- Buchner, Bas (author), Bunnik, T. (author), Andrews, J. (author), Naciri, M. (author) conference paper 2004
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- Andrews, David J. (author) conference paper 2001
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- Andrews, Chad (author) report 2001
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- Andrews, Glenn (author) conference paper 2000
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- Andrews, David J. (author) conference paper 1999
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- Andrews, D.W. (author), Durenberger, D.W. (author) report 1977
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Andrews, E.J. (author)An attempt has been made to provide a better understanding of the influence of aerodynamic characteristics on the handling qualities of amphibious hovercraft. This is the third and final report of a series of three reports in which the following have been explored. i) Aerodynamic characteristics of related hovercraft shapes; ii) the effect of...report 1971
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Andrews, D.R. (author), Sawyer, W.G. (author)The characteriatics of a 60° apex angle cone for measuring local Mach number, total pressure, and flow directions have been determined at Mach numbers of 2.47, 3.25, 3.97 and 4.32 at angles of pitch up to 29°.report 1962
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Andrews, D.R. (author), Brown, C.S. (author)Mach number and flow angle distributions in the working section of the Mach 4 nozzle of the 4 ft x 3 ft High-Supersonic-Speed Wind Tunnel are presented for a range of total pressure and humidity.report 1962