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AERADE: Recent submissions
Now showing items 3481-3498 of 3498
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Calculated Pressure Distributions for the R.A.E. 100-104 Aerofoil Sections
R. C. Pankhurst
;
H. B. Squire
(
1952
)
Approximate two-dimensional aerofoil theory part 4 the design of centre lines
S. Goldstein
(
1952
)
Designing a slot for a given wall velocity
A. Thom
;
Laura Klanfer
(
1952
)
The diffusion of transverse loads in a reinforced circular cylinder with non-rigid frames
S.R. Lewis
(
1952
)
Digital recording and analysing of flight test data a proposed system
E.J. Petherick
(
1952
)
Approximate two-dimensional aerofoil theory part 6 aerofoils with hinged flaps
S. Goldstein
;
J. H. Preston
(
1952
)
Approximate two-dimensional aerofoil theory part 5 the positions of maximum velocity and theoretical CL-ranges
S. Goldstein
(
1952
)
Draft corrections for water surface deflection under no.1 carriage of the R.A.E. seaplane tank
T.B. Owen
(
1952
)
Designing to avoid dangerous behaviour of an aircraft due to the effects on control hinge moments of ice on the leading edge of the fixed surface
D. E. Morris
(
1952
)
Approximate two-dimensional aerofoil theory part 1 velocity distributions for symmetrical aerofoils
S. Goldstein
(
1952
)
Approximate two-dimensional aerofoil theory part 3 approximate designs of symmetrical aerofoils for specified pressure distributions
S. Goldstein
;
E. J. Richards
(
1952
)
Approximate two-dimensional aerofoil theory part 2 velocity distributions for cambered aerofoils
S. Goldstein
(
1952
)
Pressure measurements in a supersonic tunnel on a two-dimensional aerofoil of R.A.E. 104 section
D. W. Holder
;
A. Chinneck
;
R. J. North
(
1951
)
The measurement of heat transfer and skin friction at supersonic speeds part 2 boundary layer measurements on a flat plate at M = 2.5 and zero heat transfer
R. J. Monaghan
;
J. E. Johnson
(
1952
)
Flight tests on the Youngman-Baynes high-lift experimental aircraft
D. Lean
(
1952
)
A theoretical and experimental investigation of the flow in a duct of varying cross-section, with particular application to the design of ducts for free flight ground-launched model tests
C.H.E. Warren
;
R.E. Dudley
;
P.J. Herbert
(
1951
)
Observations of the supersonic flow round a 6 per cent double wedge
D. W. Holder
;
A. Chinneck
;
D. G. Hurley
(
1951
)
The supersonic pressure drag of a swept wing with a cranked maximum thickness line
K. D. Thomson
(
1951
)
Now showing items 3481-3498 of 3498
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