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A theoretical analysis of the free vibration of discretely stiffened cylindrical shells with arbitrary end conditions / by D.M. Egle and K.E. Soder.
| Main Author: | Egle, D. M. |
|---|---|
| Other Authors: | Soder, K. E. |
| Language(s): | English |
| Published: |
Washington, D.C. : National Aeronautics and Space Administration ; 1969. |
| Subjects: |
Cylindrical shells.
Free vibration. Rayleigh-ritz method. Stiffness. Computer programs. Digital computers. Flexibility. Stiffening. Vibration effects. Cylindric algebras. Vibration (Aeronautics) |
| Note: |
"June 1969"--Cover. Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 11/15/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19690018786%5F1969018786.pdf. "NASA CR-1316." |
| Physical Description: |
xi, 76 p. :
ill. ;
27 cm.
|
| Original Format: | Book |
| Locate a Print Version: |
Find in a library |
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