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Showing 4 out of a total of 4 results for community: Aeronautical Research Council. (0.045 seconds)

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Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2

M. C. Neale; P. S. Lamb (1967)
Tests with a two-dimensional intake having all-external compression and a design mach number of 2.0

M. C. Neale; P. S. Lamb (1967)
Some tests with a variable ramp intake having sidewall compression and a design mach number of 2.2

M. C. Neale; P. S. Lamb (1967)
More tests with a variable ramp intake having a design mach number of 2.2

M. C. Neale; P. S. Lamb (1967)

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Author
- M. C. Neale (4)
- P. S. Lamb (4)
Date Issued
- 1967 (4)