Role of boundary conditions on flutter of orthotropic panels.

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Flutter of rectangular orthotropic panel supported by deflectional spring along two edges in supersonic airflow

Document ID

19660055300

Acquisition Source

Legacy CDMS

Document Type

Reprint (Version printed in journal)

Authors

Date Acquired

August 3, 2013

Publication Date

July 1, 1966

Publication Information

Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS

Subject Category

Accession Number

66A34590

Distribution Limits

Public

Other

Keywords

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