Review and Discussion of “the Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller‐Rotors”
Abstract:The subject and findings of this paper are of interest to the reviewers, as they have both been actively engaged in this area for, the past several years.
Document Type: Research Article
Affiliations: Bell Helicopter Company, Fort Worth, Texas
Publication date: October 1, 1967
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