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Theory of an Airplane Encountering Gusts IIIReport presents a new method for solving linear equations developed by Bromwich, which is suited to determine the motion for any particular gust, when the machine started from equilibrium, without the trouble of determining the constants of integration in the complementary function. (author)
Document ID
19930091055
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Report
Authors
Wilson, Edwin Bidwell
Date Acquired
September 6, 2013
Publication Date
January 1, 1918
Report/Patent Number
NACA-TR-27
Report Number: NACA-TR-27
Accession Number
93R20345
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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