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The longitudinal equations of motion of a tilt prop/rotor aircraft including the effects of wing and prop/rotor blade flexibilityThe equations of motion for the longitudinal dynamics of a tilting prop/rotor aircraft are developed. The analysis represents an extension of the equations of motion. The effects of the longitudinal degrees of freedom of the body (pitch, heave and horizontal velocity) are included. The results of body freedom can be added to the equations of motion for the flexible wing propeller combination.
Document ID
19760021138
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Curtiss, H. C., Jr. (Princeton Univ. NJ, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-137855
TR-1273
Accession Number
76N28226
Funding Number(s)
CONTRACT_GRANT: NSG-2045
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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