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

Browsing Aeronautical Research Council by Author "E. F. Lawlor"

Now showing items 1-1 of 1

Wind tunnel tests at Mach numbers between 0.6 and 1.4 of a 60 degrees swept wing having an aerofoil section designed for subcritical flow at a Mach number of 1.2 part 1 9 percent thick section with "triangular" pressure distribution

E. F. Lawlor (1962)

Now showing items 1-1 of 1

Search AERADE

Browse

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

My Account

Login