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The forces and moments on airplane engine mountsA resume of the equations and formulas for the forces and moments on an aircraft-engine mount is presented. In addition, available experimental data have been included to permit the computation of these forces and moments. A sample calculation is made and compared with present design conditions for engine mounts.
Document ID
19930081382
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Donely, Philip
Date Acquired
September 6, 2013
Publication Date
December 1, 1936
Report/Patent Number
NACA-TN-587
Report Number: NACA-TN-587
Accession Number
93R10672
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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