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Showing 8 out of a total of 8 results for community: Aeronautical Research Council. (0.117 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)
Some characteristics of rectangular multi-shock and isentropic external compression intakes at a mach number of 2.9

R. A. Dutton; E. L. Goldsmith (1961)
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 performance of some axi-symmetric isentropic centrebody intakes designed for Mach numbers of 2.48 and 3.27

E. L. Goldsmith; G. V. F. Smith (1966)
Half-body and wing combinations in supersonic flow a review of some principles and possibilities

E. L. Goldsmith; P. H. Cook (1965)
Boundary layer bleed drag at supersonic speeds

E. L. Goldsmith (1966)
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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Author
- E. L. Goldsmith (8)
- G. V. F. Smith (2)
- R. A. Dutton (2)
- C. S. Brown (1)
- N. A. Evans (1)
- P. H. Cook (1)
- R. T. Griffiths (1)
Date Issued
- 1967 (4)
- 1966 (2)
- 1965 (1)
- 1961 (1)