Direct formulation of a 4-node hybrid shell element with rotational degrees of freedom
By: Mohammad A. Aminpour.
Contributors: Langley Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA contractor report -- 4282.; NASA contractor report -- NASA CR-4282.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1990
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 24
Subjects: Shells (Engineering) -- Effect of strains and stresses on -- Mathematical models.; Finite element method.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-093-M.

"Prepared for Langley Research Center under Contract NAS1-18599."

Includes bibliographical references (p. 11-13).

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative ; 11 x 15 cm.

NAS1-18599. 505-63-01-10.