Return to search

Structural response and damage development of cylindrical composite panels

Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997. / Includes bibliographical references (v. 2, leaves 252-262). / by Mark A. Tudela. / Ph.D.

Identiferoai:union.ndltd.org:MIT/oai:dspace.mit.edu:1721.1/49970
Date January 1997
CreatorsTudela, Mark A. (Mark Allen)
ContributorsPaul A. Lagace., Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics
PublisherMassachusetts Institute of Technology
Source SetsM.I.T. Theses and Dissertation
LanguageEnglish
Detected LanguageEnglish
TypeThesis
Format2 v. (464 leaves), application/pdf
RightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission., http://dspace.mit.edu/handle/1721.1/7582

Page generated in 0.0011 seconds