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Comparison of calculated and measured blade loads on a full-scale tilting proprotor in a wind tunnelThe loads measured in a wind tunnel on a full-scale tilting proprotor are compared with calculated results. The data consists primarily of oscillatory beamwise bending moments at 35% radial station, oscillatory spindle chord bending moments, and oscillatory pitch link loads. The measured and calculated results as a function of thrust are compared over a range of nacelle angles from 0 to 75 deg, and a range of speeds from 80 to 185 knots.
Document ID
19800022880
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Johnson, W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1980
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
USAAVRADCOM-TR-80-A-8
NASA-TM-81228
Report Number: USAAVRADCOM-TR-80-A-8
Report Number: NASA-TM-81228
Accession Number
80N31386
Funding Number(s)
PROJECT: RTOP 505-42-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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