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Showing 10 out of a total of 28 results for collection: Aeronautical Research Council Reports & Memoranda.
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With blockage corrections in a closed wind tunnel for one or two wall-mounted models subject to separated flow
R. W. F. Gould
(
1969
)
A three-parameter family of mean velocity profiles for incompressible turbulent boundary layers with distributed suction and small pressure gradient
B. G. J. Thompson
(
1969
)
A three component gun tunnel balance designed for testing thin delta wings
T. Opatowski
(
1969
)
The theoretical treatment of slowly oscillating part-span control surfaces in subsonic flow
H. C. Garner
;
Doris E. Lehrian
(
1969
)
Further piloted simulation studies of the handling characteristics of a slender-wing supersonic transport aircraft during approach and landing
B. N. Tomlinson
;
T. Wilcock
(
1969
)
A low-speed wind-tunnel investigation of the tailplane effectiveness of a model representing the airbus type of aircraft
D. A. Lovell
(
1969
)
Calculation of the turbulent boundary layer in a vortex diffuser
T-S Cham
;
M. R. Head
(
1969
)
Published reports and memoranda of the aeronautical research council (nos. 3451 to 3550)
Aeronautical Research Council
(
1969
)
The two-dimensional characteristics of a 12.2 percent thick RAE 100 aerofoil section
D. S. Woodward
(
1969
)
Strength variability in structural materials
F. Clifton
(
1969
)
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A. W. Moore (2)
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Date Issued
1969 (28)