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Aeronautical Research Council Current Papers: Recent submissions

Now showing items 121-140 of 1393

Interference problems on wing-fuselage combinations part 3 symmetrical swept wing at zero incidence attached to a cylindrical fuselage

J. Weber; M. G. Joyce (1975)
Urea formaldehyde foamed plastic emergency arresters for civil aircraft

G. M. Gwynne (1975)
The development of portable coolers for the liquid conditioned suit

G. F. Barlow (1975)
Interference problems on wing-fuselage combinations part 4 the design problem for a lifting swept wing attached to a cylindrical fuselage

J. Weber; M. G. Joyce (1975)
Measurements of pressure distribution on a half-model wing-body combination of 55 deg. sweep over a wide range of reynolds number

K. G. Winter; J. B. Moss (1975)
Interference problems on wing-fuselage combinations part 1 lifting unswept wing attached to a cylindrical fuselage at zero incidence in midwing position

J. Weber (1975)
Interference problems on wing-fuselage combinations part 2 symmetrical unswept wing at zero incidence attached to a cylindrical fuselage at zero incidence in midwing position

J. Weber; M. G. Joyce (1975)
An assessment of the accuracy of subsonic linearized theory for the design of warped slender wings

Patricia J. Davies (1975)
Low-speed wind-tunnel tests of a two-dimensional wing fitted with two plain differentially-deflected trailing-edge flaps

John Mckie (1975)
Systems of coordinates suitable for the numerical calculation of three-dimensional flow fields

K. W. Mangler; J. C. Murray (1975)
A non-axisymmetric end-wall boundary-layer theory for axial compressor rows

J.W. Railly (1975)
Developments in the lifting surface theory treatment of symmetric planforms with a leading edge crank in subsonic flow

B.L. Hewitt; W. Kellaway (1975)
The theory of partial retraction of imperfectly elastic ropes

G.W.H. Stevens (1975)
A theoretical and experimental investigation of the external-flow, jet-augmented flap

P. R. Ashill (1975)
The characteristics of a family of rooftop aerofoils designed at their drag-rise condition in viscous, compressible flow part 1 design condition

B. G. J. Thompson; S. W. Cosby (1975)
Measurements of oscillatory aerodynamic hinge moments from the response of a wind tunnel model to turbulent flow

G. B. Hutton; D. A. Drane; D. R. Gaukroger (1975)
Observations of the flow from a rectangular nozzle

A. G. Kurn (1975)
Free-flight model dynamic stability measurements on a 'not-so-slender' wing/fin combination at zero and small lift, M = 0.8 to 2.0

G. H. Greenwood; Geraldine F. Edwards (1975)
The characteristics of a family of rooftop aerofoils designed at their drag-rise condition in viscous, compressible flow part 2 off design conditions

B. G. J. Thompson; S. W. Cosby (1975)
The effect of load dwells during fatigue crack propagation

F. E. Kiddle (1975)

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