Stability and Dynamic Analysis of a Slender Column with Curved Longitudinal Stiffeners

By National Aeronautics and Space Administration

The results of a stability design study are presented for a slender column with curved longitudinal stiffeners for large space structure applications. Linear stability analyses are performed using a link-plate representation of the stiffeners to determine stiffener local buckling stresses. Results from a set of parametric analyses are used to determine an approximate explicit expression for stiffener local buckling in terms of its geometric parameters. This expression along with other equations governing column stability and mass are assembled into a determinate system describing minimum mass stiffened column design. An iterative solution is determined to solve this system and a computer program incorporating this routine is presented. Example design problems are presented which verify the solution accuracy and illustrate the implementation of the solution routine. Also, observations are made which lead to a greatly simplified first iteration design equation relating the percent increase in column mass to the percent increase in column buckling load. From this, generalizations are drawn as to the mass savings offered by the stiffened column concept. Finally, the percent increase in fundamental column vibration frequency due to the addition of deployable stiffeners is studied. Lake, Mark S. Langley Research Center...

• Format: Paperback
• Language: English
• ISBN: 1730873219
• ISBN13: 9781730873218
• Release Date: January 1
• Publisher: Independently Published
• Length: 68 Pages
• Weight: 0.40 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"