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Showing 4 out of a total of 4 results for community: Aeronautical Research Council. (0.062 seconds)

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The drag of some wedge centre-body intakes at mach numbers of 1.56, 1.86 and 2.14

R. A. Dutton; E. L. Goldsmith (1967)
An experimental and theoretical comparison at M=4 of the lift-to-drag ratio of some possible aircraft shapes

C. S. Brown; E. L. Goldsmith (1967)
Tests at M = 1.82 on an engine installation with boundary-layer diverter for a slender gothic wing

R. T. Griffiths; E. L. Goldsmith (1967)
The effect of combined boundary-layer suction and base bleed on the drag of a 10 degree cone at M = 2.58

E. L. Goldsmith; N. A. Evans; G. V. F. Smith (1967)

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- E. L. Goldsmith (4)
- C. S. Brown (1)
- G. V. F. Smith (1)
- N. A. Evans (1)
- R. A. Dutton (1)
- R. T. Griffiths (1)
Date Issued
- 1967 (4)