Flutter Characteristics of the Slab Tail

670260

2/1/1967

Authors
Abstract
Content
The slab tail, or stabilator is a comparatively popular design feature of modern business airplanes. Unlike conventional controls, however, there are no rules nor criteria for flutter prevention for slab configurations.
The several types of flutter than can occur in a slab tail installation have been studied in the hope that a meaningful flutter criterion can be developed. Unfortunately, too many independent parameters affect the flutter characteristics for this objective to be realized. The influence of these parameters is shown, and some rules are derived which should be useful to the slab tail designer.
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DOI
https://doi.org/10.4271/670260
Citation
McKillop, J., "Flutter Characteristics of the Slab Tail," 3rd Annual Business Aircraft Conference (1967), Wichita, Kansas, United States, April 5, 1967, https://doi.org/10.4271/670260.
Additional Details
Publisher
Published
2/1/1967
Product Code
670260
Content Type
Technical Paper
Language
English