Development of an engine model for an integrated aircraft design tool
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2015. === Cataloged from PDF version of thesis. === Includes bibliographical references (pages 101-103). === This thesis describes the development of a new engine weight surrogate model and High Pressure...
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Format: | Others |
Language: | English |
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Massachusetts Institute of Technology
2015
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Online Access: | http://hdl.handle.net/1721.1/98811 |