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Browsing Aeronautical Research Council (1945-1979) by Author "P. S. Lamb"

Now showing items 1-6 of 6

Further tests with a variable ramp intake having a design mach number of 2.2

M. C. Neale; P. S. Lamb (1966)
More tests with a variable ramp intake having a design mach number of 2.2

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)
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)
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 variable ramp intake having combined external/internal compression, and a design mach number of 2.2

M. C. Neale; P. S. Lamb (1965)

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