Clyde Warsop
BAE Systems
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Publication
Featured researches published by Clyde Warsop.
26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference | 2008
Graham Andrew Johnson; Martyn John Hucker; Harriet Ann Holden; Caroline Trigg; Clyde Warsop
As part of a large UK project called “Integrated Wing, Flight Physics, Technology Validation Programme”, BAE Systems have been further developing their hot-film sensors constructed using silicon manufacturing techniques with the ultimate aim of making them capable of being certified for flight. Primarily, this has involved looking at aspects of the sensor design, such as the robustness of the sensors to impacts and their resistance to environmental degradation. Tests done to date have shown that provided the sensors have a thin protective coating of a few microns thickness and are not installed close to the leading-edge of a wing they should be capable of being certified for flight.
Measurement & Control | 2012
Graham Andrew Johnson; Martyn John Hucker; C. Morley; Clyde Warsop
BAE Systems have been developing hot-film sensors for the detection and monitoring of laminar/turbulent flow on a wing. The sensors are constructed using silicon manufacturing techniques, with the ultimate aim of making them capable of being certified for flight. Primarily, this has involved looking at aspects of the sensor design, such as the robustness of the sensors to raindrop impacts and their resistance to environmental degradation. Tests done to date have shown that provided the sensors have a thin protective coating of a few microns thickness and are not installed close to the leading-edge of a wing they should be capable of being certified for flight.
10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference | 2010
Graham Andrew Johnson; Martyn John Hucker; Dave Gough; Dave Baker; Clyde Warsop
Previous research at BAE Systems has developed a MEMS based hot-film sensor that can be flush mounted into a surface with sub-surface connections. The work described in this paper covers the development of a device that integrates this MEMS sensor, with an integrated, miniaturized constant temperature anemometer circuit, and a miniaturized laminar/turbulent flow detection circuit. Attention has also been paid to addressing how this might be incorporated into an aircraft structure and systems. The ultimate aim is a flightworthy sensor that includes all the necessary components into a single package of the order of a few cm 3 , which only requires three wires - power, earth and data, and which can easily be integrated into an aircraft structure.
Flow Turbulence and Combustion | 2007
Shan Zhong; Mark Jabbal; Hui Tang; Luis Garcillan; F Guo; Norman Wood; Clyde Warsop
Flow Turbulence and Combustion | 2007
Hui Tang; Shan Zhong; Mark Jabbal; Luis Garcillan; F Guo; Norman Wood; Clyde Warsop
Archive | 2008
Martyn John Hucker; Clyde Warsop; Graham Andrew Johnson; David W. Gough
Flow Turbulence and Combustion | 2007
Clyde Warsop; Martyn John Hucker; Andrew Julian Press; Paul James Dawson
Archive | 2004
Clyde Warsop; Mark Watson; Artur Jerzy Jaworski
Archive | 2007
Martyn John Hucker; Clyde Warsop; Harriet Ann Holden
Archive | 2007
Michael Victor Cook; Clyde Warsop