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Showing 4 out of a total of 4 results for collection: Aeronautical Research Council Reports & Memoranda.
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Experiments with a two-dimensional aerofoil designed to be free from turbulent boundary-layer separation at small angles of incidence for all mach numbers
D. W. Holder
;
R. F. Cash
(
1957
)
An experimental investigation of leading-edge flow separation from a 4 per cent thick two-dimensional biconvex aerofoil
B. D. Henshall
;
R. F. Cash
(
1957
)
Observations of the flow past a two-dimensional 4 per cent thick biconvex aerofoil at high subsonic speeds
B. D. Henshall
;
R. F. Cash
(
1957
)
Observations of the flow patterns of two-dimensional 4 per cent thick biconvex aerofoil at Mo = 1.40 and 1.63
B. D. Henshall
;
R. F. Cash
(
1957
)
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R. F. Cash (4)
B. D. Henshall (3)
D. W. Holder (1)
Date Issued
1957 (4)