Browsing CoA. Reports by Title

Browsing CoA. Reports by Title

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  • Heiba, A. E. (College of Aeronautics, Cranfield., 1982-10)
    The paper presents an experimental study of natural frequencies and modes of vibration of uniform cantilever plates. Sixteen planforms are tested by combining aspect ratios of 0.8, 1.2, 1.6 and 2 with leading edge sweep-back ...
  • Radok, J. R. M. (College of Aeronautics, Cranfield, 1951-04)
    The equation of motion of a uniform swept box with stringers and ribs are deduced. For the case of vibrations of a cantilever they are transformed into integrated equations, an approximate method of solution of which is indicated.
  • Toro, E. F. (1991)
    We present Numerical Viscosity Functions, or NVFs, for use with Riemann-problem based shock-capturing methods as applied to viscous flows. In particular, viscous flux limiters are derived. The analysis pertain to a linear ...
  • Robinson, A. (College of Aeronautics, Cranfield., 1950-05)
    The field of flow due to a shock wave or explanation wave undergoes a considerable modification in the neighbourhood of a rigid wall. It has been suggested that the resulting propagation of the disturbance upstream is ...
  • Kirkby, S.; Robinson, A. (College of Aeronautics, Cranfield, 1947-04)
    The increment in lift due to wing-body interference at supersonic speed is calculated approximately for an untapered wing without sweepback.

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