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Aircraft optimization by a system approach
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:107622
Physical properties of the Benchmark Models Program supercritical wing
Joyner Library
- Microforms B300
Call Number:
NAS 1.15:4457
Aircraft design through service experience
Joyner Library
- Fed Docs Stacks
Call Number:
C 31.138:103
Investigation of compressive strength of spruce struts of rectangular cross section and derivation of formulas suitable for use in airplane design
Joyner Library
- Microforms B300
Call Number:
CIS US EXEC MF C13.8-152
Investigation of compressive strength of spruce struts of rectangular cross section and derivation of formulas suitable for use in airplane design
Joyner Library
- Microforms B300
Call Number:
CIS US EXEC MF C13.8-152
Proposed handbook for airplane designers (commercial).
Joyner Library
- Microforms B300
Call Number:
C23.6-2.1