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Theoretical Investigation of the Subsonic and Supersonic Flutter Characteristics of a Swept Wing Employing a Tuned Sting Mass Flutter Suppressor.

机译：采用调谐质量颤振抑制器的扫掠翼的亚音速和超声颤振特性的理论研究。

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摘要

Flutter calculations were based on the modified strip-analysis method of NACA Research Memorandum L57L10 and covered Mach numbers from 0 to 1.75. The flutter suppressor consists of a small mass connected to the wing by means of a flexible sting. This system may be considered analogous to the spring-mass type of vibration absorber frequently used on heavy rotating machinery. Three suppressor masses were investigated but no attempt was made to make the configuration optimum.

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作者
Yates, E. C.;
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年度 1960
页码 1-50
总页数 50
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Flutter analysis; Subsonic flutter; Supersonic flutter; Swept wings; Vibration; Mach number; Rotation; Suppressors;

机译：颤振分析;亚音速颤振;超音速颤振;扫掠翅膀;振动;马赫数;旋转;抑制器;

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专利

1. Numerical Investigation into Flutter and Flutter-Buffet Phenomena for a Swept Wing and a Curved Planform Wing [J] . Chiarelli Mario Rosario, Bonomo Salvatore International journal of aerospace engineering . 2019,第PTa1期

机译：横掠机翼和弯曲平面机翼的颤振和颤振-布菲现象的数值研究
2. Numerical Investigation into Flutter and Flutter-Buffet Phenomena for a Swept Wing and a Curved Planform Wing [J] . Chiarelli Mario Rosario, Bonomo Salvatore International journal of aerospace engineering . 2019,第PTa1期

机译：扫翼扑翼和颤动自助式现象的数值调查及弯曲平面翼
3. Numerical Investigation into Flutter and Flutter-Buffet Phenomena for a Swept Wing and a Curved Planform Wing [J] . Mario Rosario Chiarelli, Salvatore Bonomo International journal of aerospace engineering . 2019,第4期

机译：扫翼扑翼和颤动自助式现象的数值调查及弯曲平面翼
4. Transonic and Supersonic Nonlinear Flutter Characteristics of a Swept-Back Composite Wing Model [C] . Dong-Hyun Kim, Jae-Han Yoo, In Lee International conference on composite materials . 2001

机译：扫回复合翼模型的跨音和超声波非线性颤动特性
5. Investigation of carbon rod stiffeners for wing flutter mitigation on a supersonic business jet. [D] . Simmons, Frank, III. 2004

机译：研究用于减轻超音速公务机机翼颤振的碳棒加强件。
6. On fluttering modes for aircraft wing model in subsonic air flow [O] . Marianna A. Shubov -1

机译：亚音速气流中机翼模型的颤振模式
7. Theoretical investigation of the flutter characteristics of supersonic cascades with subsonic leading-edge locus [O] . Bell James Keith 1975

机译：亚音速前沿轨迹的超音速叶栅颤动特性的理论研究
8. SOME EFFECTS OF VARIATIONS IN DENSITY AND AERODYNAMIC PARAMETERS ON THE CALCULATED FLUTTER CHARACTERISTICS OF FINITE-SPAN SWEPT AND UNSWEPT WINGS AT SUBSONIC AND SUPERSONIC SPEEDS [R] . Yates, E. C., Jr. 1960

机译：密度和气动参数变化对有限跨越和超音速下有限跨度和非长翼计算颤振特性的影响

Theoretical Investigation of the Subsonic and Supersonic Flutter Characteristics of a Swept Wing Employing a Tuned Sting Mass Flutter Suppressor.

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