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Stability equations for airship hullsIn the text are derived simple formulae for determining, directly from the data of wind tunnel tests of a model of an airship hull, what shall be the approximate character of oscillation, in pitch or yaw, of the full-scale airship when slightly disturbed from steady forward motion. (author)
Document ID
19930091279
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Zahm, A F
Date Acquired
September 6, 2013
Publication Date
January 1, 1926
Report/Patent Number
NACA-TR-212
Report Number: NACA-TR-212
Accession Number
93R20569
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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