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Aerodynamic characteristics at Mach numbers from 2.5 to 3.5 of a canard bomber configuration designed for supersonic cruise flight

机译：设计用于超音速巡航飞行的鸭式轰炸机配置的马赫数为2.5至3.5的空气动力学特性

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Carmel, Melvin R; Kelly, Thomas C; Gregory, Donald T;
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年度 1958
页码 1-54
总页数 54
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. METHOD OF COMPUTATION OF AERODYNAMIC CHARACTERISTICS OF THE WING-TAIL CONFIGURATION IN TRANSONIC CRUISE FLIGHT [J] . L.L. Teperin, L.N. Teperina, Myo Thein TsAGI science journal . 2018,第6期

机译：跨音巡航飞行中翼尾结构的空气动力学特性计算方法
2. Aerodynamic Characteristics of Canard-Forward Swept Wing Aircraft Configurations [J] . G. Q. Zhang, S. C. M. Yu, A. Chien, Journal of Aircraft . 2013,第2期

机译：卡纳德前掠机翼构型的空气动力学特性
3. Influence of Gurney flaps on aerodynamic characteristics of a canard-configuration aircraft [J] . Wei Zhongcheng, Zhan Jingxia, He Xi, Aircraft engineering . 2019,第4期

机译：格尼襟翼对鸭式飞机的空气动力学特性的影响
4. AERODYNAMIC DESIGN OF SINGLE-EXPANSIONRAMP NOZZLE FOR AIRCRAFT WITH SUPERSONIC CRUISE SPEED OF FLIGHT [C] . A.V. Shenkin, A.P. Mazurov, A.P. Bykov Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：飞行器超音速飞行器单膨胀进气口气动设计
5. Aircraft conceptual design study of the canard and threesurface unconventional configurations for the purposes of reducing environmental impacts [D] . Desharnais, Olivier 2014

机译：为了减少环境影响，对鸭翼和三面非常规配置进行飞机概念设计研究
6. Experimental investigation on the characteristics of supersonic fuel spray and configurations of induced shock waves [O] . Yong Wang, Yu-song Yu, Guo-xiu Li, -1

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7. Aerodynamic flow characteristics of utilizing delta wing configurations in supersonic and subsonic flight regimes [O] . Ruffels William, Dakka Sam 2016

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Aerodynamic characteristics at Mach numbers from 2.5 to 3.5 of a canard bomber configuration designed for supersonic cruise flight

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