Observations of the flow over a two-dimensional 4 per cent thick aerofoil at transonic speeds
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Observations of the flow over a two-dimensional 4 per cent thick aerofoil at transonic speeds
B. D. Henshall
;
R. F. Cash
URI:
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3748
Date:
1959
Abstract:
Flow photographs and detailed pressure distributions for a 4 per cent thick circular-arc biconvex aerofoil at transonic speeds are presented. The results for incidences of 0, 1, 2 and 5 deg are analysed in detail.
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Aeronautical Research Council Reports & Memoranda
[1313]
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