Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds : supersonic leading and trailing edges

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Document ID

19930082815

Acquisition Source

Legacy CDMS

Document Type

Other

Authors

Date Acquired

August 16, 2013

Publication Date

May 1, 1950

Report/Patent Number

Accession Number

93R12105

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

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