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Showing 10 out of a total of 42 results for collection: Aeronautical Research Council Reports & Memoranda. (0.139 seconds)

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A numerical solution of an integral equation satisfied by the velocity distribution around a body of revolution in axial flow

D. Kershaw (1961)
Pressure-plotting and force tests at mach numbers up to 2.8 on an uncambered slender wing of p = .50, S/Co = .25 'handley page ogee'

A. L. Courtney; A. O. Ormerod (1961)
On the numerical evaluation of the drag integral

Evelyn Eminton (1961)
Aerodynamic derivative measurements on a wing with a horn-balanced control surface

P. R. Guyett; J. K. Curran (1961)
Measurements of pitching-moment derivatives for blunt-nosed aerofoils oscillating in two-dimensional supersonic flow

P. G. Pugh; L. Woodgate (1961)
A theoretical analysis of the stability of an aeroplane on northerly headings when controlled by an aileron-steering autopilot monitored from a gyro-magnetic compass

H. R. Hopkin; M. R. Watts; D. E. Fry (1961)
On the flexure of thin built-up wings

G. G. Pope (1961)
The aerodynamic forces on an oscillating two-dimensional wing in accelerated supersonic flight

D. E. Davies (1961)
The use of a deep electrolytic tank as a lifting-surface calculator

H. S. Ward (1961)
Further experimental investigations of the characteristics of cambered gothic wings at mach numbers from 0.4 to 2.0

L. C. Squire (1961)

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- 1961 (42)