Boeing Helicopter, together with other United States helicopter manufacturers, participated in a finite element applications program to emplace in the United States a superior capability to utilize finite element analysis models in support of helicopter airframe design. The activities relating to planning and creating a finite element vibrations model of the Boeing Model 36-0 composite airframe are summarized, along with the subsequent analytical correlation with ground shake test data.
Plan, Formulate, Discuss and Correlate a Nastran Finite Element Vibrations Model of the Boeing Model 360 Helicopter Airframe
1989
296 pages
Report
No indication
English