Browsing CoA. Memoranda by Title

Browsing CoA. Memoranda by Title

Sort by: Order: Results:

  • 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 ...
  • Preliminary studies of the time-dependent shear and uniaxial tensile behaviour of oriented polymers 
    Clayton, D. (College of Aeronautics, 1969-02)
    Summary The work reported in this memo is the initial stages of an investigation of the time-dependent behaviour of certain anisotropic polymers. In the first instance low density polyethylene with a transversely ...
  • A progress report on the evaluation of metal cutting coolants 
    Chater, T. (College of Aeronautics, 1965-12)
    An intensive investigation into the grinding process was carried out in The College of Aeronautics Machine Tools Laboratory during 1955-6. The outcome of this work was a method of evaluating the efficiency of grinding ...
  • Progress report to sponsors in the surfacing division, The Welding Institute 
    Apps, R. L. (College of Aeronautics, 19)
    Since the last report to sponsors circulated in mid-1967, considerable concern has been felt over the wide scatter of results. The scatter in results between specimens produced in a single batch was generally ...
  • Project report on airport location 
    The College of Aeronautics Transport Short Course, Transport Short Course (College of Aeronautics, 1968)
    An integral part of the two week transport short course was a group project study by course members, applying material presented on the course to a practical problem in transport systems analysis. Airport location in ...
  • Project report on Milton Keynes 
    College of Aeronautics, Transport Short Course (College of Aeronautics, 1969)
    Introduction 1.1.1 This is a project report written by the members of the College of Aeronautics short course held between 24th February and 7th March, 1969. 1.1.2 An Interim Report was presented by the Planning ...
  • Push-pull fatigue properties of wires in an iridium - 5% tungsten alloy 
    Clifton, T. E.; Whitbread, R. C. (College of Aeronautics, 1965-11)
    Introduction This memorandum reports a series of tests to determine the fatigue properties of an iridium - 5% tungsten alloy at 600°c and 700°C. A previous memorandum, Memo. Mat. 61, reports the fatigue properties at ...
  • The pyrolytic degradation of epoxy resins in nitrogen at 400 to 700 degrees C 
    Bishop, D. P.; Smith, D. A. (College of Aeronautics, 1969-03)
    The thermal degradation of a bisphenol-A based epoxy resin (EP 274) cured with 4,4’ -diaminodiphenyl methane (DDM) and with phthalic anhydride (PA) was studied using pyrolysis gas chromatography. Conclusive evidence for ...

Search CERES


Browse

My Account