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Aeronautical Research Council Current Papers: Recent submissions

Now showing items 861-880 of 1393

Measurements of the pitching moment derivatives for rigid wings of rectangular plan form oscillating about the mid-chord axis in supersonic flow

C. Scruton et al (1961)
Reduction of lift-dependent drag with separated flow

G. H. Lee (1959)
On the control of shock-induced boundary-layer separation with discrete air jets

R. A. Wallis; C. M. Stuart (1958)
The 7 in. x 7 in. hypersonic wind tunnel at R.A.E. Farnborough parts 1, 2 and 3

J.F.W. Crane; L.F. Crabtree (1962)
An experimental investigation of the characteristics of an ogee wing from M = 0.4 to M = 1.8

L.C. Squire; D.S. Capps (1962)
Problems associated with the use of a false wall as a reflection plane for half model tests in the de Havilland high speed wind tunnel

D. R. Holder; H. C. Farley (1962)
The estimation of transient temperature distributions and thermal stresses in turbine and compressor discs

M. Cox (1961)
Subjective response to sonic bangs

M. J. Clarke; J. F. Wilby (1962)
Observations of Stall Cells in a Single Stage Compressor

J. Durham (1962)

A specially developed pressure-measuring instrument has been used to observe instantaneous values of the pressure, velocity and direction of the flow in a single stage, low hub-tip ratio, axial compressor. During stall ...
Surface oil-flow patterns on wings of different leading-edge radius and sweepback

H. C. Garner; D. K. Cox (1961)
Gusts at low altitude in North Africa

N. I. Bullen (1962)
An amplitude probability analyser for use in turbulence and noise measurements

R. F. Johnson (1962)
Wind tunnel tests at Mach numbers between 0.6 and 1.4 of a 60 degrees swept wing having an aerofoil section designed for subcritical flow at a Mach number of 1.2 part 1 9 percent thick section with "triangular" pressure distribution

E. F. Lawlor (1962)
A survey of buffeting loads

Diana M. Seal (1959)
An investigation into the effects of ground proximity on twin coaxial annular jets, using hotand cold air

R. V. Barrett; J. C. Tipping (1960)
The design and testing of a low range acceleration transducer with predictable response characteristics

I. McLaren (1961)
Scale models for thermo-aeroelastic research

W. G. Molyneux (1961)
Low-speed pressure-plotting tests on a flat-plate m-wing fitted with part-span nose-flaps

L.A. Wyatt; G.P. Ilott (1961)
Low-speed wind-tunnel tests on sharp-edged gothic wings of aspect-ratio .75

R. F. A. Keating (1961)
Turbulence encountered by ambassador aircraft over Europe

J. R. Heath-Smith (1960)

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