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Static Stability Characteristics of a 0.16- Scale Model of a Jet-Lift V/STOL Research Airplane in Cruise

机译：巡航中Jet-Lift V / sTOL研究飞机0.16比例模型的静态稳定特性

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作者
Winston, M. M.;
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年度 1969
页码 1-2
总页数 2
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Jet lift ; Static stability ; V/stol aircraft ; Wind tunnel stability tests ; Cruising flight ; Graphs (charts) ; Horizontal tail surfaces ; Tail assemblies;

机译：喷气式升降机;静态稳定性; V / stol飞机;风洞稳定性试验;巡航飞行;图形（图表）;水平尾翼表面;尾部组件;

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1. Definition system and Criteria related to the static stability of airplanes (theird report) -static sideslip stability, static roll stability, and static yaw stability- [J] . Osamu Kobayashi Transactions of the Japan society for aeronautical and space sciences . 2002,第148期

机译：与飞机的静态稳定性有关的定义系统和标准（其后继报告）-静态侧滑稳定性，静态侧倾稳定性和静态偏航稳定性-
2. Definition system and criteria related to the static stability of airplanes (first report) -definition system, static flight speed stability, and static angle of attack stability- [J] . osamu Kobayashi Transactions of the Japan society for aeronautical and space sciences . 2002,第148期

机译：与飞机静态稳定性有关的定义系统和标准（首次报告）-定义系统，静态飞行速度稳定性和静态攻角稳定性-
3. Definition system and criteria related to the static stability of airplanes (second Report) - static pitch stability- [J] . Osamu Kobayashi Transactions of the Japan society for aeronautical and space sciences . 2002,第148期

机译：与飞机静态稳定性有关的定义系统和标准（第二次报告）-静态俯仰稳定性-
4. Computational AeroAcoustics of Counter Rotating Open Rotor Model on rear full scale airplane in cruise condition [C] . Thomas Le Garrec, Gabriel Reboul AIAA aeroacoustics conference;AIAA/CEAS aeroacoustics conference . 2012

机译：后方全尺寸飞机巡航状态下反向旋转旋翼模型的计算航空声学
5. A FUEL-EFFICIENT CRUISE PERFORMANCE MODEL FOR GENERAL AVIATION PISTON ENGINE AIRPLANES. [D] . PARKINSON, RICHARD CHARLES HALLAM. 1982

机译：通用航空活塞发动机飞机的燃油效率巡航性能模型。
6. Aerodynamic Characteristics of a Feathered Dinosaur Measured Using Physical Models. Effects of Form on Static Stability and Control Effectiveness [O] . Dennis Evangelista, Griselda Cardona, Eric Guenther-Gleason, -1

机译：使用物理模型测量的羽毛恐龙的空气动力学特性。形式对静态稳定性和控制有效性的影响
7. Propulsion System and Airframe Integration for Jet-Lift V/STOL Airplanes [O] . H. A. Weber, Aadu Karemaa 1972

机译：喷气机V / STOL飞机的推进系统和机身集成
8. Static stability characteristics of a 0.16- scale model of a jet-lift V/STOL research airplane in cruise [R] . Winston, M. M. 1969

机译：喷射升力V / sTOL研究飞机的0.16比例模型的静态稳定性特征

Static Stability Characteristics of a 0.16- Scale Model of a Jet-Lift V/STOL Research Airplane in Cruise

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