Browsing Aeronautical Research Council Reports & Memoranda by Author "G. A. Naylor"

Browsing Aeronautical Research Council Reports & Memoranda by Author "G. A. Naylor"

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  • G. A. Naylor (1942)
    This report shows that the application of classical flutter theory to the determination of wing flexural-torsional flutter speeds is considerably simplified by the omission of a term which is usually the very small difference ...
  • G. A. Naylor; Anne Pellew (1942)
    This note deals with binary aileron-spring-tab flutter involving rotation of the aileron and spring tab about their hinge lines. The methods of R. & M. 1155 are used to calculate the variation of flutter speed with various ...
  • G. A. Naylor (1942)
    Oscillation of control-surface tabs has occurred in flight. General experience and the investigations of this report suggest that the oscillations were flutter, involving translation of the tab, arising from bending of the ...

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