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R. F. Cash

National Physical Laboratory

12

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26

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Design and operating features of the N.P.L. 6 in. shock tunnel

1965
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Preliminary measurements in a shock tunnel of shock angle and undersurface pressure related to a nonweiler wing

1963
- L. Pennelegion
- R. F. Cash
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Observations of the flow over a two-dimensional 4 per cent thick aerofoil at transonic speeds

1959
- B. D. Henshall
- R. F. Cash
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Observations of the flow past a two-dimensional 4 per cent thick biconvex aerofoil at high subsonic speeds

1957
- B. D. Henshall
- R. F. Cash
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An experimental investigation of leading-edge flow separation from a 4 per cent thick two-dimensional biconvex aerofoil

1957
- B. D. Henshall
- R. F. Cash
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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

1957
- D. W. Holder
- R. F. Cash
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Observations of the flow patterns of two-dimensional 4 per cent thick biconvex aerofoil at Mo = 1.40 and 1.63

1957
- B. D. Henshall
- R. F. Cash
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Tests at high subsonic speeds on a 10 per cent thick pressure-plotting aerofoil of RAE 104 section

1951
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