AERADE Home
→
Aeronautical Research Council
→
Browsing Aeronautical Research Council by Author

Browsing Aeronautical Research Council 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)

Now showing items 1-6 of 6

Search AERADE

Browse

All of AERADE
This Community
- By Issue Date
- Authors
- Titles
- Subjects

My Account

Login