The use of NASTRAN in propulsion system structural integration analysis is described. Computer support programs for modeling, substructuring, and plotting analysis results are discussed. Requirements on interface information and data exchange by participants in a NASTRAN substructure analysis are given. Static and normal modes vibration analysis results are given with comparison to test and other analytical results.
NASTRAN applications to aircraft propulsion systems
1975-09-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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AIAA | 1974
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|Structural analysis of light aircraft using NASTRAN
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