A Study of the Problem of Designing Airplanes With Satisfactory Inherent Damping of the Dutch Roll Oscillation ; NACA Technical Reports

"Considerable interest has recently been shown in means of obtaining satisfactory stability of the dutch roll oscillation for modern high-performance airplanes without resort to complicated artificial stabilizing devices. One approach to this problem is to lay out the airplane in the earliest stages of design so that it will have the greatest practicable inherent stability of the lateral oscillation. The present report presents some preliminary results of a theoretical analysis to determine the design features that appear most promising in providing adequate inherent stability" (p. 1).

Verfasser: Campbell, John P.
McKinney, Marion O., Jr.
Dokumenttyp: Report
Erscheinungsdatum: 1954
Schlagwörter: aircraft stability / Dutch roll oscillations / aircraft control
Sprache: Englisch
Permalink: https://search.fid-benelux.de/Record/base-27451725
Datenquelle: BASE; Originalkatalog
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Link(s) : https://digital.library.unt.edu/ark:/67531/metadc65560/