Parameters which have influence upon weight of thin wall pressure vessels under specified design conditions are examined; generalized treatment is presented of governing primary weight equation that relates structural configuration efficiency, material efficiency, and prescribed design conditions; configuration efficiencies of various shapes for different failure criteria are summarized and compared; structural strength/weight ratios attained with current monolithic metallics and filamentary composites are evaluated; design synthesis chart summarizes major results of investigation.
Comparative efficiencies of aerospace pressure vessel design concepts
AIAA J
AIAA Journal ; 4 , n 12
1966
9 pages
Aufsatz (Zeitschrift)
Englisch
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Aerospace pressure vessel design synthesis
TIBKAT | 1965
|Aerospace pressure vessel design synthesis
NTRS | 1965
|Aerospace Pressure Vessel Design Synthesis
NTIS | 1965
|