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Showing 10 out of a total of 41 results for collection: Aeronautical Research Council Reports & Memoranda. (0.196 seconds)

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The Calculation of the Loading and Pressure Distribution on Cranked Wings

G. G. Brebner (1953)
The harmonically oscillating wing with finite vortex trail

P. F. Jordan (1953)
An analysis of steady straight flight with inclined thrust

S. B. Gates; A. W. Thorpe (1953)
The R.A.E. electronic simulator for flutter investigations in six degrees of freedom or less

F. Smith; W. D. T. Hicks (1953)
Some flutter tests on swept-back wings using ground-launched rockets

W. G. Molyneux; F. Ruddlesden (1953)
Gust alleviation factor. Parts I, II and III

J. K. Zbrozek (1953)
Measurements of the direct pitching-moment derivatives for three wing planforms at high subsonic speeds

J. B. Bratt; W. G. Raymer; J. E. G. Townsend (1953)
An unconventional type of fatigue-testing machine

F. Aughtie; H. L. Cox (1953)
Hinge-moment derivatives for an oscillating control

C. S. Sinnott (1953)
Model testing technique employed in the R.A.E. seaplane tank

T. B. Owen; A. G. Kurn; A. G. Smith (1953)

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- 1953 (41)