Effect of yaw at supersonic speeds on theoretical aerodynamic coefficients of thin pointed wings with several types of trailing edge

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Document ID

19930082351

Acquisition Source

Legacy CDMS

Document Type

Other

Authors

Date Acquired

August 16, 2013

Publication Date

March 1, 1948

Report/Patent Number

Accession Number

93R11641

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

Keywords

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Type

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