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
01.09.1975
Aufsatz (Konferenz)
Keine Angabe
Englisch
Structural analysis of light aircraft using NASTRAN
AIAA | 1974
|Structural analysis of light aircraft using NASTRAN
NTRS | 1973
|Fuzzy Structures Analysis of Aircraft Panels in NASTRAN
NTRS | 2001
|Fuzzy Structures Analysis of Aircraft Panels in NASTRAN
NTIS | 2001
|