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Showing 10 out of a total of 31 results for collection: Aeronautical Research Council Reports & Memoranda. (0.18 seconds)

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A general method (depending on the aid of a digital computer) for deriving the structural influence coefficients of aeroplane wings Parts 1 and 2

D. Williams (1956)
Experiments on two-dimensional base flow at M = 2.4

L. Fuller; J. Reid (1956)
Experiments on Pitot-Tubes in Shear Flow

F. A. MacMillan (1956)
The matrix force method of structural analysis and some new applications

J. H. Argyris; S. Kelsey (1956)
The theoretical determination of normal modes and frequencies of vibration

I. T. Minhinnick (1956)
A theoretical and experimental investigation of the flow over a family of rectangular wings of biconvex section at M = 1.42

R. C. Lock (1956)
Operational formulae for response calculations

S. Neumark (1956)
A subsonic lifting-surface theory for low-aspect-ratio wings

C. R. Taylor (1956)
Aerodynamic characteristics of rectangular wings of small aspect ratio

I. J. Campbell; C. F. Blanks; D. A. Leaver (1956)
Supersonic wind-tunnel flutter tests of two rectangular wings

P. R. Guyett (1956)

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- 1956 (31)