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Publication


Featured researches published by Clyde Warsop.


26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference | 2008

Development of MEMS Hot-film Sensors for use in the Integrated Wing Project

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

Development of MEMS Hot-Film Sensors

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

Development of a MEMS based Integrated Hot-film Flow Sensor

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

Towards the design of synthetic-jet actuators for full-scale flight conditions : Part 1: The fluid mechanics of synthetic-jet actuators

Shan Zhong; Mark Jabbal; Hui Tang; Luis Garcillan; F Guo; Norman Wood; Clyde Warsop


Flow Turbulence and Combustion | 2007

Towards the design of synthetic-jet actuators for full-scale flight conditions Part 2: Low-dimensional performance prediction models and actuator design method

Hui Tang; Shan Zhong; Mark Jabbal; Luis Garcillan; F Guo; Norman Wood; Clyde Warsop


Archive | 2008

Fluid flow monitoring

Martyn John Hucker; Clyde Warsop; Graham Andrew Johnson; David W. Gough


Flow Turbulence and Combustion | 2007

Pulsed Air-jet Actuators for Flow Separation Control

Clyde Warsop; Martyn John Hucker; Andrew Julian Press; Paul James Dawson


Archive | 2004

Method of controlling vortex bursting

Clyde Warsop; Mark Watson; Artur Jerzy Jaworski


Archive | 2007

Millimetre-scale engine

Martyn John Hucker; Clyde Warsop; Harriet Ann Holden


Archive | 2007

Flow control actuators

Michael Victor Cook; Clyde Warsop

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