Browsing CoA. Memoranda by Title

Browsing CoA. Memoranda by Title

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  • M. S. 760 'Paris' response to atmospheric turbulence 
    Clarke, B. S. (College of Aeronautics, 1967)
    This report describes work carried out at The College of Aeronautics, Cranfield, during the first year of a contract to study the effects of atmospheric turbulence on the M.S.76O % Paris' aircraft. The aircraft was ...
  • Manufacturing techniques using dycril 
    Morrison, W. (College of Aeronautics, 1967)
    Fluidic elements are manufactured in various ways such as injection moulding, epoxy casting and from photo-sensitive ceramic and plastics. Most of the initial work on elements has been carried out using Dycril because ...
  • A mathematical model for handling in a warehouse 
    Kay, E. (College of Aeronautics, 1967-03)
  • The measurement of biaxial strains in coated fabric materials using the disc-replica method 
    Webb, J.; Richards, D. M. (College of Aeronautics, 1969-09)
    A method of measuring biaxial strains in coated fabric type materials is presented whereby the strain is deduced from the distortion of a circular impression made on the material. The impression is placed on the ...
  • The mechanical properties of anisotropic polymers 
    Unknown author (College of Aeronautics, 1966-10)
    This report, in conjunction with that for the previous six months, forms the complete first year report for the period 1st October, 1965 to 31st September, 1966. Detailed results on the stress-strain properties of ...
  • The mechanical properties of anisotropic polymers 
    Darlington, M. (College of Aeronautics, 1966)
    The work in this period can conveniently be split into two parts which are reported separately. Part I is concerned with experimental work on the stress-strain properties of anisotropic polythene. This work was initiated ...
  • The mechanical properties of anisotropic polymers: progress report no. 3 
    Darlington, M. W. (College of Aeronautics, 1967-03)
  • The mechanical properties of anisotropic polymers: progress report no. 5 
    Darlington, M. W. (College of Aeronautics, 1968-03)
    A report of work carried out during the period 1st October, 1967, to 31st March, 1963.
  • The mechanical properties of anisotropic polymers: Progress report no. 6 
    Darlington, M. W. (College of Aeronautics, 1968-09)
    Part 1 General Developments The basic development work on the tensile creep apparatus was completed by March, 1968. A description of the latest 'heavy-duty' creep rig and two types of contraction extensometer, together ...
  • The mechanical properties of anisotropic polymers: progress report no. 7 
    Darlington, M. W. (College of Aeronautics, 1969-03)
    Part I General Developments The major part of the period under review was devoted to a study of the tensile creep properties of isotropic and uniaxially oriented Perspex sheets (standard grade) using the three heavy-duty ...
  • Milton Keynes - preliminary estimates of regional traffic flows in 1981 
    Lennox, S. G.; Tidbury, Joan; Clark, J. M. (College of Aeronautics, 1967)
    The Milton Keynes Development Corporation and their planning consultants have asked the College Transport Group to investigate the scale of likely regional traffic flows into and out of Milton Keynes. At this stage the ...
  • Milton Keynes: an outline cost-benefit study 
    Lennox, S. G.; Tidbury, Joan (College of Aeronautics, 1968)
    This is a preliminary survey of some of the factors which would need to be investigated in the design and cost-benefit analysis of alternative transport systems for Milton Keynes. It outlines the framework within ...
  • A new approach to the prediction of tool wear 
    Cherry, J. (College of Aeronautics, 1967-07)
    Tool life is of major concern for economical production in the metal cutting industries and a simple method of predictive the tool wearability of materials would be of considerable value in enabling optimum cutting conditions ...
  • A non-equilibrium kinetic description of shock wave structure 
    Battat, D. (College of Aeronautics, 1968-06)
    A formulation for the shock wave structure is devised by viewing the transition as a phenomenon in which non-equilibrium effects play an important role. The essence of the method is the approximation of Boltzmann's ...
  • Notes on the feasibility of automatic warehousing 
    Kay, E.; Pemberton, A. W. (College of Aeronautics, 1968-10)
    There is now sufficient information and experience available on the subject of automatic warehousing to make it possible for an organisation with major storage problems to assess the advantages and disadvantages of ...
  • The numerical evaluation of the grinding process and the basic mechanics of grinding wheel wear 
    Purcell, John (College of Aeronautics, 1965)
    During the production process development for the manufacture of an experimental supersonic aircraft , an unusual and difficult grinding problem was encountered. Arising from the experimental work carried out to solve this ...
  • Optimisation of factors influencing the efficiency of finish machining operations 
    Enahoro, H. E. (College of Aeronautics, 19)
    Optimum machining conditions were determined for various materials, steels, cast irons, brasseses, bronzes and an aluminium alloy. Surface finish readings were taken with the Sigmatex and the Surtronic and values of 10 ...
  • Optimum stiffness inflated mattress beams 
    Webb, J. (College of Aeronautics, 1969-09)
    This report considers primarily the relatively short cantilever type of inflated matresss beam, currently being employed as sidebody structure on some hovercraft. The rib pitch for optimum stiffness/weight of such beams ...
  • The philosophy and principles of welding design 
    Jubb, J. E. M. (College of Aeronautics, 1967)
    The welding designer requires a philosophy for his design responsibilities and a thorough understanding of the basic principles in the subjects covering his responsibilities. The education of the welding designer must ...
  • Pilot reliability investigation: final report on agreement PD/28/035/ADM 
    Robertson, I. A. (College of Aeronautics, 1966)
    The feasibility of constructing a device to give a measure of pilot reliability has been investigated. A rig to meet the proposals made by BLEU has been designed and basic circuits constructed and tested for accuracy ...

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