Browsing CoA. Memoranda: Aero (1964-1968) by Title

Browsing CoA. Memoranda: Aero (1964-1968) by Title

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  • Effect of engine, tank and propellant specific cost on single stage recoverable booster economics 
    Carton, Dennis S. (College of Aeronautics, 1964)
    Reusable first stages using hydrogen-oxygen, hydrogen-fluorine and kerosine-oxygen are compared with non-reusable stages using a solid in addition to the liquid combinations. The criterion used for comparison is the ...
  • Non-equilibrium flow in plane expansion waves 
    Cleaver, J. W. (College of Aeronautics, 1964-06)
    The non-equilibrium supersonic flow of a relaxing or reacting gas through a plane expansion has been studied from a numerical,, analytical and experimental point of view. The flow of an ideal dissociating gas in a two ...
  • A note on the decay of aircraft trailing vortices 
    Lilley, G. M. (College of Aeronautics, 1964-03)
    An elementary theory of aircraft trailing vortex decay is presented based on an assumed law for the variation of the mean eddy viscosity with distance from the wing. This law is based on the experimental data of Rose ...
  • Optimum structures 
    Hemp, W. S.; Chan, H. S. Y. (College of Aeronautics, 1965-07)
    The design of the best structure for a given purpose depends upon the criterion used for optimisation. Structures may be designed to safely transmit a given system of forces using the least weight of material.. They may ...
  • Shock wave structure in highly rarefied flows 
    Battat, D. (College of Aeronautics, 1964-07)
    The Boltzmann equation is written in terms of two functions associated with the gain and loss of a certain type of molecule due to collisions. Its integral form is then applied to the problem of normal shock structure, and ...
  • Structural testing of wooden aircraft 
    College of Aeronautics, (Cranfield) (College of Aeronautics, 1964-12)
    For some years now the structural integrity of wooden aircraft of timber and glued plywood torsion box construction has been a matter of concern to the Air Registration Board since it is impossible to assess, by inspection, ...
  • Various optimisation methods for preliminary cost and mass distribution assessment for multistage rocket vehicles 
    Kalitventzeff, B. (College of Aeronautics, 1964)
    Preliminary staging studies of multi-stage space launchers are described. Both propellant and thrust scaling factors are used, and also cost parameters for propellant, propellant scaling units and thrust scaling units. ...

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