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AERADE: Recent submissions
Now showing items 3281-3300 of 3498
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Flutter calculations on a rudder with trailing-edge spoiler
Ll. T. Niblett
(
1956
)
A note on derivative apparatus for the N.P.L. 9.5-inch high speed tunnel
J. B. Bratt
(
1956
)
Base pressures in supersonic flow
G. E. Gadd
;
D. W. Holder
;
J. D. Regan
(
1956
)
Aerodynamic derivatives for two cropped delta wings and one arrowhead wing oscillating in distortion modes
D. L. Woodcock
(
1956
)
The hot-wire anemometer for turbulence measurements part 4
B. Wise
;
D. L. Schultz
(
1956
)
Some experiments on an effusion cooled turbine nozzle blade
S. J. Andrews
;
H. Ogden
;
Jane Marshall
(
1956
)
The hot-wire anemometer for turbulence measurements part 3
B. Wise
;
D. L. Schultz
(
1956
)
Boundary layer separation in two-dimensional supersonic flow
G. E. Gadd
;
D. W. Holder
(
1956
)
Measurement of lift, pitching moment and hinge moment on a two-dimensional cusped RAE.102 aerofoil
A. S. Batson
(
1956
)
The hot-wire anemometer for turbulence measurements part 1
B. Wise
(
1956
)
The Hot-Wire Anemometer for Turbulence Measurements Part II
B. Wise
;
D. R. Stewart
(
1956
)
An account is given of some experimental work undertaken to test the theory of operation of a hot-wire anemometer with radio-frequency heating, which has been given in a previous paper.
A theoretical investigation of the factors affecting stalling flutter of compressor blades
A. D. S. Carter
(
1955
)
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
)
Now showing items 3281-3300 of 3498
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