Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings - NASA Technical Reports Server (NTRS)

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Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings

Document ID

19930082522

Acquisition Source

Legacy CDMS

Document Type

Other

Authors

Date Acquired

August 16, 2013

Publication Date

March 1, 1949

Report/Patent Number

Accession Number

93R11812

Distribution Limits

Public

Copyright

Work of the US Gov. Public Use Permitted.

Keywords

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Type

19930082522.pdf

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