Research Catalog

Postbuckling delamination of a stiffened composite panel using finite element methods

Title
  1. Postbuckling delamination of a stiffened composite panel using finite element methods / S. Natsiavas, C.D. Babcock and W.G. Knauss.
Published by
  1. Pasadena, California : California Institute of Technology, August, 1987.
Author
  1. Natsiavas, S.

Details

Additional authors
  1. Babcock, Charles D.
  2. Knauss, Wolfgang Gustav
  3. California Institute of Technology, issuing body.
  4. United States. National Aeronautics and Space Administration, sponsoring body.
Description
  1. 9, 10 unnumbered pages : illustrations.
Series statement
  1. NASA/CR ; 182803
Uniform title
  1. NASA contractor report ; NASA CR-182803.
Subject
  1. Buckling
  2. Delaminating
  3. Finite element method
  4. Compression loads
  5. Plate theory
Call number
  1. GPO Microfiche NAS 1.26:182803
Note
  1. "August, 1987."
  2. "GALCIT SM report 87-19."
Bibliography (note)
  1. Includes bibliographical references (pages 8-9).
Reproduction (note)
  1. Microfiche.
Funding (note)
  1. Sponsored by the National Aeronautics and Space Administration
Author
  1. Natsiavas, S., author.
Title
  1. Postbuckling delamination of a stiffened composite panel using finite element methods / S. Natsiavas, C.D. Babcock and W.G. Knauss.
Publisher
  1. Pasadena, California : California Institute of Technology, August, 1987.
Type of content
  1. text
Type of medium
  1. microform
Type of carrier
  1. microfiche
Series
  1. NASA/CR ; 182803
  2. NASA contractor report ; NASA CR-182803.
Bibliography
  1. Includes bibliographical references (pages 8-9).
Reproduction
  1. Microfiche. [Washington, D.C.] : [National Aeronautics and Space Administration], 1988. 1 microfiche : negative.
Funding
  1. Sponsored by the National Aeronautics and Space Administration [NSG-1483]
  2. [GALCIT-SM-87-19]
Added author
  1. Babcock, Charles D., author.
  2. Knauss, Wolfgang Gustav, author.
  3. California Institute of Technology, issuing body.
  4. United States. National Aeronautics and Space Administration, sponsoring body.
Other form:
  1. Print version: Natsiavas, S. Postbuckling delamination of a stiffened composite panel using finite element methods (OCoLC)83324455
  2. Online version: Natsiavas, S. Postbuckling delamination of a stiffened composite panel using finite element methods (OCoLC)908252076
Gpo item no.
  1. 0830-H-14 (MF)
Sudoc no.
  1. NAS 1.26:182803
View in legacy catalog