NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Appendix: Results obtained to dateOptimization procedures are described for the rotor blade design process by integrating appropriate disciplines and accounting for important interactions among the disciplines. Progress is reported in the areas of aerodynamic performance optimization, dynamic optimization, optimum placement of tuning masses for vibration reduction, and structural optimization. Selected results from these activities are highlighted in this appendix.
Document ID
19900003272
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Walsh, Joanne L.
(NASA Langley Research Center Hampton, VA, United States)
Chattopadhyay, Aditi
(NASA Langley Research Center Hampton, VA, United States)
Pritchard, Jocelyn I.
(NASA Langley Research Center Hampton, VA, United States)
Nixon, Mark W.
(Army Aviation Systems Command Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1989
Publication Information
Publication: Integrated Multidisciplinary Optimization of Rotorcraft: A Plan for Development
Subject Category
Aircraft Design, Testing And Performance
Accession Number
90N12588
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available