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Aeronautical Research Council Current Papers: Recent submissions

Now showing items 961-980 of 1393

Effects of design speed and normal acceleration on aircraft structure weight

M.E. Burt (1960)
A wind tunnel investigation into the factors affecting the spanwise load distribution over the vertical tail surface of an aircraft having a wedge-type rear fuselage

K. F. S. Chard; J. Deakin; A. R. Collar (1960)
A turbine nozzle cascade for cooling studies part 1 the measurement of mean nusselt numbers at the blade surface

R. I. Hodge (1960)
A comparison between the measured and predicted cooling performance of an internally spanwise ventilated turbine nozzle blade

R. I. Hodge (1960)
Tests on a .03 scale model of the vickers M.T.1000 (C.132D) in the compressed air tunnel, N.P.L

C. J. W. Miles; R. C. Fox (1960)
Simulation of visual flight, with particular reference to the study of flight instruments

J. M. Naish (1960)
Calculation of the recoil of a shock tube

B. A. Woods (1960)
Aspects of insect contamination in relation to laminar flow aircraft

I. G. C. Lachmann (1960)
Some tests on cascades of compressor blades fitted with vortex generators

R. Staniforth (1960)
An investigation at transonic speeds of the performance of various distributed rougness bands used to cause boundary-layer transition near the leading edge of a cropped delta half-wing

E.W.E. Rogers et al (1960)
Visualization of secondary flow in the reservoirs of the slotted - wall working sections of the A.R.L. 12-inch and 30-inch water tunnels

D. A. E. Leaver (1960)
The rotating flap as a high-lift device

L. F. Crabtree (1960)
The effect of fuselage modifications on the zero-lift transonic drag of a fighter aircraft (hunter F. Mk.1) as measured by free-flight model tests

G. H. Greenwood (1960)
Some measurements in the vortex flow generated by a sharp leading edge having 65 degrees sweep

N. C. Lambourne; D. W. Bryer (1960)
The longitudinal frequency response to elevator of an aircraft over the short period frequency range

D. M. Ridland (1960)
Wind tunnel tests on the flutter of a swept and unswept wing with ailerons

H. Hall; J.A. Rein (1960)
Measurements of the effect of surface cooling on boundary layer transition on a 15 degrees cone part 2 tests at M = 3 and M = 4 in the 5 in. x 5 in. no. 5 wind tunnel at R.A.E. Farnborough

J. G. Woodley (1960)
Free-flight experiments on the measurement of free-stream static pressure at transonic speeds with particular reference to the Mk.9 pitot-static head

C. Kell (1960)
Note on conditions for which data on the power spectra at atmospheric turbulence are required

J. K. Zbrozek; F. Pasquill (1960)
Some instabilities arising from the interactions between shock waves and boundary layers

N. C. Lambourne (1960)

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