Calculated Subsonic Span Loads and Resulting Stability Derivatives of Unswept and 45 Degrees Sweptback Tail Surfaces in Sideslip and in Steady Roll - NASA Technical Reports Server (NTRS)

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Calculated Subsonic Span Loads and Resulting Stability Derivatives of Unswept and 45 Degrees Sweptback Tail Surfaces in Sideslip and in Steady Roll

Document ID

19930083928

Acquisition Source

Legacy CDMS

Document Type

Other

Authors

Date Acquired

August 16, 2013

Publication Date

October 1, 1954

Report/Patent Number

Accession Number

93R13218

Distribution Limits

Public

Copyright

Work of the US Gov. Public Use Permitted.

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Type

19930083928.pdf

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