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Aeronautical Research Council: Recent submissions
Now showing items 2581-2600 of 2786
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Calibration of the flow in the working section of the 3 ft x 3 ft tunnel, National Aeronautical Establishment
D. E. Morris
(
1956
)
Flow direction measurements in supersonic wind tunnels
D. J. Raney
(
1956
)
Boundary layer measurements on 10 degrees and 20 degrees cones at M = 2.45 and zero heat transfer
F. V. Davies
;
J. R. Cooke
(
1956
)
Some advantages and disadvantages of variable and non-linear gearing between the pilot's control and the control surface
D. A. Lang
(
1956
)
An experimental investigation of the blade vibratory stresses in a single stage compressor
A. D. S. Carter et al
(
1956
)
Wind tunnel tests on antisymmetric flutter of a delta wing with rolling body freedom
D. R. Gaukroger
;
D. Nixon
(
1955
)
Some fatigue characteristics of a two spar light alloy structure (meteor 4 tailplane)
K. D. Raithby
;
Jennifer Longson
(
1956
)
Fatigue loadings in flight loads in the tailplane and fin of a varsity
Anne Burns
(
1956
)
Saunders-Roe princess flying boat G-alun air and water handling tests
Marine Aircraft Experimental Establishment
(
1956
)
Models for aero-elastic investigations
H. Templeton
(
1955
)
Flutter calculations on a resonance model delta wing
H. Hall
(
1955
)
Additional data on surface slopes of the RAE 100 - 104 aerofoil sections
Edna M. Love
;
J. Williams
(
1955
)
Measurements of pitching moment derivatives for a series of rectangular wings at low wind speeds
P. R. Guyett
;
D. E. G. Poulter
(
1955
)
The strength of tubes under uniform external pressure
P.C. Cleaver
(
1955
)
Relative accuracy of deflections and bending moments (or stresses) derived by the method of RAE report no. structures 168
D. Williams
(
1956
)
Preliminary Low Speed Wind Tunnel Tests on Flat Plates and Air Brakes: Flow, Vibration and Balance Measurements
R. Fail
;
T. B. Owen
;
R. C. W. Eyre
(
1956
)
List of current papers published by the Aeronautical Research Council (numbers 201-250)
Aeronautical Research Council
(
1956
)
Tests of Humidity Effects on Flow in a Wind Tunnel at Mach Numbers between 2.48 and 4
R. J. Monaghan M.A.
(
1956
)
Turbulence encountered by comet 1 aircraft
J.R. Heath-Smith
(
1956
)
The theoretical wave drag of open-nose axisymmetrical forebodies with varying fineness ratio, area ratio and nose angle
J.H. Willis
;
D.G. Randall
(
1956
)
Now showing items 2581-2600 of 2786
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