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Investigation of a 1/22-scale model of the Republic F-105 airplane in the Langley 8-foot transonic tunnel : static longitudinal stability and control and performance characteristics at transonic speeds

机译：在兰利8英尺跨音速隧道中对共和国F-105飞机的1/22比例模型进行调查：跨音速时的静态纵向稳定性和控制以及性能特征

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Luoma, Arvo A;
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年度 1956
页码 1-125
总页数 125
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. NUMERICAL INVESTIGATIONS OF THE EFFECT OF AEROELASTIC DEFORMATIONS OF THE WING ON THE AERODYNAMIC CHARCATERISTICS OF THE HALF-MODEL OF AN AIRPLANE AT TRANSONIC SPEED [J] . V. A. Barinov, O. V. Pavlenko, V. V. Yanin TsAGI science journal . 2016,第3期

机译：机翼气动变形对跨音速飞机半模气动特性影响的数值研究
2. Investigation of winglet on the transonic flutter characteristics for a wind tunnel test model CHNT-1 [J] . Lv Binbin, Lu Zhiliang, Guo Tongqing, Aerospace science and technology . 2019,第MARa期

机译：基于CHNT-1风洞试验模型的小翼对跨音速颤振特性的研究
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. Experimental Investigations of the NASA Common Research Model in the NASA Langley National Transonic Facility and NASA Ames 11-Ft Transonic Wind Tunnel (Invited) [C] . Melissa B. Rivers, Ashley Dittbeme AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2011

机译：NASA兰利国家跨音速设施和NASA Ames 11-Ft跨音速风洞中的NASA通用研究模型的实验研究（邀请）
5. Initial investigations of transonic turbine aerodynamics using the Carleton University High-Speed Wind Tunnel. [D] . Jeffries, Michael Scott. 2001

机译：使用卡尔顿大学高速风洞进行跨音速涡轮空气动力学的初步研究。
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. Experimental Investigations of the NASA Common Research Model in the NASA Langley National Transonic Facility and NASA Ames 11-Ft Transonic Wind Tunnel (Invited) [O] . Rivers S. M., Dittberner Ashley 2011

机译：NASA兰利国家跨音速设施和NASA Ames 11-Ft跨音速风洞中的NASA通用研究模型的实验研究（邀请）

Investigation of a 1/22-scale model of the Republic F-105 airplane in the Langley 8-foot transonic tunnel : static longitudinal stability and control and performance characteristics at transonic speeds

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