Supersonic Flutter of a Cylindrical Shell with Application to the Centaur Interstage Adapter

Analytic solution to flutter boundaries of circular cylindrical shell subjected to supersonic flow with application to Centaur interstage adapter

Document ID

19660010162

Acquisition Source

Legacy CDMS

Document Type

Contractor Report (CR)

Authors

Date Acquired

August 3, 2013

Publication Date

January 1, 1963

Subject Category

Report/Patent Number

Accession Number

66N19451

Funding Number(s)

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

Keywords

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Type

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