Browsing by Author "Radok, J. R. M."

Browsing by Author "Radok, J. R. M."

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  • Radok, J. R. M. (College of Aeronautics, Cranfield, 1952-03)
    Using oblique coordinates, the static problems of Aero-elasticity for swept wings are reduced to the solution of integral – or matrix equations, which may be solved by iteration. The present treatment also indicates the ...
  • Radok, J. R. M. (College of Aeronautics, Cranfield, 1952-04)
    Using oblique coordinates, integro-differential equations of motion of aircraft with swept wings are deduced from Hamilton’s Principle for the dynamic problems of aero-elasticity, i.e. for the problems of free vibrations, ...
  • Radok, J. R. M. (College of Aeronautics, Cranfield, 1952-06)
    Using a new approach to the theoretical study of thin-walled cylinders with discrete reinforcing members developed in the paper, the problem of general instability of such structures is solved with more than usual generality. ...
  • 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.