Publikationsdatum:
2019-08-17
Beschreibung:
The writer sets out to prove by calculation and experiment that by extensive utilization of the skin to carry axial load (reduction of stringer spacing) the stringer sections can be made small enough to afford a substantial saving in structural weight. This saving ranges from 5 to about 40 percent.
Schlagwort(e):
Aircraft Design, Testing and Performance
Materialart:
NACA-TM-1031
,
Luftfahrtforschung; 18; 9; 331-337
Format:
application/pdf
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