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Force, static longitudinal stability, and control characteristics of a 1/16-scale model of the Bell XS-1 transonic research airplane at high Mach numbers

机译：高马赫数下Bell Xs-1跨音速研究飞机的1/16比例模型的力，静态纵向稳定性和控制特性

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Mattson, Axel T; Loving, Donald L;
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年度 1948
页码 1-51
总页数 51
原文格式 PDF
正文语种 eng
中图分类工业技术;
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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. Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing [J] . Junli Wang AIP Advances . 2019,第4期

机译：低纵横比后掠翼的跨音速静态气动弹性和纵向气动特性
4. ANALYSIS OF STATIC AND DYNAMIC AEROELASTIC CHARACTERISTICS OF AIRPLANE IN TRANSONIC FLOW [C] . S. Kuzmina, O. Karas, F. Ishmuratov, Congress of the International Council of the Aeronautical Sciences . 2012

机译：跨音速流动中飞机的静态和动态气动弹性特征分析
5. Reduced static lateral stability in airplanes. [D] . Williams, Russell Loy. 2005

机译：降低了飞机的静态横向稳定性。
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. Mach number effects on transonic aeroelastic forces and flutter characteristics [O] . Yang Henry T. Y., Batina John T., Mohr Ross W. 1988

机译：马赫数对跨音速气动弹性力和颤振特性的影响

Force, static longitudinal stability, and control characteristics of a 1/16-scale model of the Bell XS-1 transonic research airplane at high Mach numbers

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