Aircraft wings automated preliminary structural design and weight determination procedures based on external shape, aerodynamic loads and fuel mass interaction
Procedure for automating aircraft wing structural design
CONFERENCE ON ELECTRONIC COMPUTATION ; 1970 ; LAFAYETTE, IN
01.01.1971
Sonstige
Keine Angabe
Englisch
Emerald Group Publishing | 2001
Moldless composite aircraft wing structural design modifications
Tema Archiv | 1991
|Structural Optimization Design of an Aircraft Metal-Composite Wing
Tema Archiv | 2013
|