Interlaminar stress analysis of dropped-ply laminated plates and shells by a mixed method
By: Peter N. Harrison, Eric R. Johnson, James H. Starnes.
Contributors: Johnson, Eric R.; Starnes, James H.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-196851.
Publisher: Virginia Polytechnic Institute and State University; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: Blacksburg, Va; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Axisymmetric bodies.; Boundary value problems.; Cylindrical shells.; Finite difference theory.; Interlaminar stress.; Laminates.; Loads (Forces); Plates (Structural members); Ply orientation.; Reissner theory.; Runge-Kutta method.; Stress analysis.; Stress distribution.
Other titles: Interlaminar stress analysis of dropped ply laminated plates and shells by a mixed method.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0069-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.