Browsing CoA. Memoranda by Title

Browsing CoA. Memoranda by Title

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  • Davis, J. A.; Loeb, H. W. (College of Aeronautics, 1965-11)
    A general method for the solution of the nonlinear Shockley-Poisson differential equation which governs the potential distribution in non-degenerate semiconductor systems is described which can be applied to the ...
  • Andrew, R.; Loeb, H. W. (College of Aeronautics, 1967-01)
    The e::tension of the resistance network analogue method to the study of a M.O.S.T. structure is described. By means of an iterative technique, data regarding channel current, field distribution, surface charge and position ...
  • Bishop, D. P.; Moffitt, B. R.; Smith, D. A. (College of Aeronautics, 1968-11)
    Pyrolysis gas chromatography and radioactive tracer techniques have been used independently to study the thermal degradation of polymers. In these laboratories the two techniques have been combined to elucidate some of ...
  • Younger, A. (College of Aeronautics, 1965-11)
    The revised approach to the measurement of the rate of crack propagation in light alloys has entailed the development of new experimental techniques, in particular the development of a multi-channel interval timer. ...
  • Loxham, J. (College of Aeronautics, 1967)
    The extensive programne of research undertaken by the Department of Production and Industrial .1.0.ministration at the College of Aeronautics, Cranfield into Metrology and Precision Engineering has shown the need for a ...
  • Dootson, M. (College of Aeronautics, 1969)
    Synopsis: This paper describes the tensile creep behaviour of fibre reinforced plastics under a uniaxial stress system. In particular, unidirectionally and bidirectionally reinforced plastics are considered for the ...
  • Darlington, M. W.; Saunders, D. W. (College of Aeronautics, 1969)
    The enhancement of many of the mechanical properties of thermoplastics which may be achieved by orienting the molecules has been known for some time. It has been exploited in the production of textile fibres end oriented ...
  • Tidbury, G. H. (College of Aeronautics, 1968-11)
    This report gives in detail the calculation of the distribution of forces in an integral structure by the matrix force method. The design of a full scale structure to test the theoretical results is described in an ...
  • Powell, E. A.; Boshier, G. C. (College of Aeronautics, 1967)
    This report outlines the aims of the project and procedures used to bring it to a successful conclusion. It also summarises the results of an investigation into the parameters which govern the specification of ...
  • Whitfield, D. (College of Aeronautics, 1965)
    This project is a practical exercise in system design undertaken by the previously named group of Electrical and Control Engineering students. The object of the project is the practical embodiment of ergonomic and systems ...
  • Melsom, A. (College of Aeronautics, 1968)
    Starting from the initial concept of a small Numerically Controlled lathe, a measurement and actuation system has been developed. An 'absolute" fluidic control system with rotary and linear encoders has been chosen and ...
  • Powell, N. (College of Aeronautics, 1968)
    This report outlines the design of a precision turning machine with a limited milling facility which incorporates a fluidic numerical control system. It contains an introduction to the project together with summaries ...
  • College of Aeronautics, (Cranfield) (College of Aeronautics, 1969)
    1. INTRODUCTION The design of an automatic assembly machine with versatility in application was undertaken as a group project by post-graduate students attending a course in production technology. This report summarises ...
  • College of Aeronautics, (Cranfield) (College of Aeronautics, 19)
    This report describes the approach to the design of an automatic versatile assembly machine of modular construction. Details of the design of the conveyor module, the platen upon which the assembly is mounted and the ...
  • Scarffe, M. F. (College of Aeronautics, 1968-06)
    A survey has been made to determine the factors influencing the design of a precision turning machine with limited milling facilities. Seventy six replies were received, have been analysed and histograms plotted and ...
  • Jones, R. V. (College of Aeronautics, 1968)
    This report outlines the design of a versatile low cost 'Precision Turning Machine with a Limited Milling Facility' which automatically produces work accurately to the required fora at a high production rate. The moving ...
  • Unknown author (College of Aeronautics, 1965-02)
    The study deals mainly with engineering problems associated with the introduction of a noise generating facility on 'Lincoln' aircraft R.F.342 for the purpose of studying the effect of high intensity sound pressure ...
  • Boshier, G. C.; Pike, G. W. H. (College of Aeronautics, 1967)
    This report outlines the design of the Drill Head for a numerically controlled drilling machine. The Committee chose to employ a nydraulic main spindle drive. As a result of the problems experienced by Wadkin Limited, ...
  • Sutcliffe, R. S.; Morrison, W. (College of Aeronautics, 1967)
    This report outlines the recommendations of the Frame Design Committee for the final design of the machine, each major part of the structure being considered individually in the following sections : 1. Worktables 2. ...
  • Norster, E. R. (College of Aeronautics, 1964-09)
    Studies have been made into the behaviour of rotating drums as a means of atomisation and fuel injection for gas turbine engines. Radial holes in the wall of the drum discharge liquid continuously, forming jets which ...

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