• Aerodynamic characteristics of two low aspect ratio rectangular wings at Mach 2 

  Marson, G. B. (College of Aeronautics, 1956-04)

  This note summarises the important results of a detailed experimental investigation into the flow and pressure distribution over two rectangular single wedge wings. The experiments were carried out .in the 9" x 9" ...
• Characteristics of the high temperature mechanisms of creep and recovery in graphite: part 3 

  College of Aeronautics, (Cranfield) (College of Aeronautics, 1963-04)

  The research reported in this document has been made possible through the support and sponsorship of the U.S. Department of the Army, through its European Research Office. This report, not necessarily in final form, is ...
• Relationship between the limits of fit determined from B.S. 1916 and the functional requirements for interference fits 

  Scarr, A. J. (College of Aeronautics, 1963-04)

  Introduction When a designer wishes to choose a shaft and hole deviation and tolerances, as, for example, an interference fit, he may be led to assume, when reading B.S.1916, that a particular fit combination will give ...
• Large scale metrology 

  Scarr, A. J. (College of Aeronautics, 1963-04)

  Introduction This interim note covers some of the problems encountered in the measurement of large sizes, up to 80 inches (200 mm), during investigations carried out at the College of Aeronautics. A description of a ...
• Some thoughts on a proposed in-flight experiment to study the effect of external noise on a swept laminarised wing 

  Hyde, D. (College of Aeronautics, 1963-04)

  A transducer-horn arrangement has been suggested as a suitable noise source to be installed in the Lancaster aircraft so that the Handley-Page suction fin could be subjected to large acoustical disturbances. The object ...
• Characteristics of the high temperature mechanisms of creep and recovery in graphite 

  College of Aeronautics, (Cranfield) (College of Aeronautics, 1963)

  The research reported in this document has been made possible through the support and sponsorship of the U.S. Department of the Army, through its European Research Office. This report, not necessarily in final form, is ...
• Characteristics of the high temperature mechanisms of creep and recovery in graphite 

  College of Aeronautics, (Cranfield) (College of Aeronautics, 1962)

  The research reported in this document has been made possible through the support and sponsorship of the U.S. Department of the Army, through its European Research Office. This report, not necessarily in final form, ...
• Ergonomics in machine tool design: second progress report on M.T.I.R.A. research project 

  Easterby, R. S. (College of Aeronautics, 1963-04)

  This report is the second of a series of reports, to be issued every six months, describing the progress of a research project on ergonomics in relation to machine tool design. The report covers, in broad outline, the ...
• Ergonomics in machine tool design: first progress report on M.T.I.R.A. research project 

  Easterby, R. S. (College of Aeronautics, 1962-10)

  This report is the first of a regular series of reports to be issued describing the progress of a research project on Ergonomics in relation to Machine Tool Design. The project is being carried out in the Ergonomics ...
• The free-molecule flow characteristics of concave surfaces 

  Pratt, M. J. (College of Aeronautics, 1963-06)

  The problem of free molecule flow over concave surfaces is investigated, and general equations formulated for the lift, drag, and heat transfer characteristics of such surfaces. The effect of multiple reflections is ...
• A low-constraint, high-pressure air feed system for wind tunnel balances 

  Alexander, A. J. (College of Aeronautics, 1963-10)

  A high-pressure air feed system, suitable for use with blowing models mounted on a six-component virtual-centre balance, is described. Air is supplied to the balance by a flexible ring main feed so that no air is lost ...
• Teaching machines for teaching work study 

  Wiltshire, H. C. (College of Aeronautics, 1963-05)

  Machines which have been used successfully for the teaching of work measurement practices are described. Although designed to shorten the period of instruction for beginners) they appear to be suitable for postgraduate ...
• The effect of nitrogen in alpha-iron on ferromagnetic domain boundary movement examined by a mechanical damping method 

  Steward, M. J. (College of Aeronautics, 1963-05)

  The effect of ageing below 200°C on the hysteresis loss in a-iron containing nitrogen has been investigated. The extent to which nitrogen is removed from solid solution during ageing, and the domain boundary hindrance ...
• The design of a hydrostatic lubrication arrangement for the horizontal and transverse slides of a no. 3 archdale vertical milling machine 

  Loxham, J. (College of Aeronautics, 1963-05)

  The Department of Production and Industrial Administration of The College of Aeronautics has made a detailed analysis into the performance of numerically controlled machine tools, and this shows that when these machines ...
• A measurement of the radiated noise on a subsonic jet aircraft in gliding flight 

  Hyde, D. (College of Aeronautics, 1963-06)

  The noise radiated from a gliding subsonic jet aircraft was measured in flight by a probe microphone installed in a ‘laminarised’ boom projecting from the fin of the aircraft. As the signal associated with the windmilling ...
• Non-newtonian flow in incompressible fluids. Part 3: some problems in transient flow 

  Kaye, A. (College of Aeronautics, 1963-06)

  N/A
• The acquisition of high speed skills. First progress report on D.S.I.R. research project 

  Whitfield, D. (College of Aeronautics, 1963-04)

  N/A
• Grinding theory 

  Hillier, M. J. (College of Aeronautics, 1962-09)

  This report presents a review and extension of current grinding theory. Grinding operations are classified on the basis of (a) the cutting action of the grit, (b) the geometry of wheel and work, (c) the type of chip ...
• Non-Newtonian flow in incompressible fluids: part 1: a general rheological equation of state: part 2: some problems in steady flow 

  Kaye, A. (College of Aeronautics, 1962-10)

  N/A
• Some tests on a circular ground effect machine with forward speed 

  Harris, T. M. (College of Aeronautics, 1962-10)

  Wind tunnel tests have been made on a circular-wing with 90° downward peripheral blowing both in and out of ground effect. Tests made with two slot widths, a range of blowing pressures and choked jets, indicate that Cu ...

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