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AERADE: Recent submissions
Now showing items 3421-3440 of 3498
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A relaxation treatment of shock waves
L. C. Woods
(
1953
)
Design of a right-angled bend with constant velocities at the walls
A. S. Thom
(
1953
)
Air cooling methods for gas turbine combustion systems
F. J. Bayley
(
1953
)
Tests on an axial compressor with various stator blade staggers
R.A. Jeffs
;
E.L. Hartley
;
P. Rooker
(
1953
)
The theory of aerofoils with hinged flaps in two-dimensional compressible flow
L. C. Woods
(
1953
)
Curves for estimating the wave drag of some bodies of revolution, based on exact and approximate theories
L. E. Fraenkel
(
1953
)
The performance of some typical turbo-jet engine exhaust systems, with particular reference to the effects of swirl
P.F. Ashwood
;
P.J. Fletcher
(
1953
)
An analysis of the air flow through the nozzle blades of a single stage turbine
I.H. Johnston
(
1953
)
Surface slopes and curvatures of the RAE 100-104 and other rooftop-type aerofoil sections
J. Williams
;
Edna M. Love
(
1953
)
Note on the lift slope, and some other properties, of delta and swept-back wings
E. F. Relf
(
1953
)
Method for the determination of the pressure distribution over a finite thin wing at a steady low speed
G. J. Hancock
(
1953
)
Pressure error measurement using the formation method
K.C. Levon
(
1953
)
Higher harmonics of flapping on the helicopter rotor
W. Stewart
(
1953
)
Effect of mean stress on the fatigue strength of D.T.D. 364 round bars with and without transverse holes
G.M. Norris
(
1953
)
The definitions of the angles of incidence and of sideslip
C.H.E. Warren
(
1953
)
Growth of the turbulent wake close behind an aerofoil at incidence
D. A. Spence
(
1953
)
The estimation of skin temperatures attained in high speed flight
F.V. Davies
;
R.J. Monaghan
(
1953
)
The low speed performance of a helicopter
A. L. Oliver
(
1953
)
A method for calculating pressure distributions on circular arc ogives at zero incidence at supersonic speeds, using the Prandtl-Meyer flow relations
H. K. Zienkiewicz
(
1953
)
An approximate method of deriving the transient response of a linear system from the frequency response
C.A.A. Wass
;
E.G. Hayman
(
1953
)
Now showing items 3421-3440 of 3498
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