This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Some Special Investigation Areas in Light Aircraft Flutter
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1972 by SAE International in United States
Annotation ability available
A brief description is given of one approach taken by a manufacturer of light business and personal aircraft to the flutter analysis of propeller whirl flutter, twin-boom aircraft, T-tail configuration, servo tabs, and all-moving tail. Effects of structural variations that may occur in the service life of an aircraft are presented, and the effect of ice formation on control surfaces is discussed.
|An Inexpensive, Full-Scale Aircraft Fatigue Test System
|IAR-46 JAR-VLA International Certification
|Concorde, Fifteen Years on the Front Line
CitationPate, C., Punatar, M., and Winn, R., "Some Special Investigation Areas in Light Aircraft Flutter," SAE Technical Paper 720309, 1972, https://doi.org/10.4271/720309.
- Reed, W. H. III Bland S. R. “An Analytical Treatment of Aircraft Propeller Precession Instability.” National Aeronautics and Space Administration January 1961
- Reed, W. H. III “Review of Propeller-Rotor Whirl Flutter.” National Aeronautics and Space Administration July 1967
- Sewall J. L. “An Analytical Trend Study of Propeller Whirl Instability.” National Aeronautics and Space Administration April 1962
- Baldock J. C. A. “The Determination of the Flutter Speed of a T-Tail Unit by Calculations, Model Tests and Flight Flutter Tests.” North Atlantic Treaty Organization Paris October 1958