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Aerodynamic characteristics of a 1/8-scale powered model of a high-speed bomber with a dual pusher propeller aft of the empennage

机译：高速轰炸机的1/8比例动力模型的空气动力学特性带有双推进器尾翼的尾翼螺旋桨

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Schnurbusch, Alfred W;
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年度 1945
页码 1-95
总页数 95
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
GROUND EFFECT - WIND TUNNEL TESTS; STABILITY & CONTROL - DOUGLAS B-42; AIRPLANES - DOUGLAS B-42 (EXPERIMENTAL) WIND TUNNEL TESTS -AAL (10' X 7') (AMER; WIND TUNNEL TESTS - AAL (10'X 7');

机译：地面效应 - 风洞隧道测试;稳定性和CONTROL - DOUGLas B-42;飞机 - 道格拉斯B-42（实验）风洞测试-aaL（10'X 7'）（美国;风洞测试 - aaL（10'X 7'）;

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1. Aerodynamic and Aeroacoustic Analysis of Installed Pusher-Propeller Aircraft Configurations [J] . Jianping Yin, Arne Stuermer, Marco Aversano Journal of Aircraft . 2012,第5期

机译：已安装的推进器-螺旋桨飞机配置的空气动力学和空气声学分析
2. APIAN-INF: an aerodynamic and aeroacoustic investigation of pylon-interaction effects for pusher propellers [J] . Tomas Sinnige, Daniele Ragni, Anwar M. N. Malgoezar, CEAS Aeronautical Journal . 2018,第2期

机译：APIAN-INF：对推进器螺旋桨塔架相互作用的空气动力学和空气声学研究
3. Aerodynamic model of propeller-wing interaction for distributed propeller aircraft concept [J] . Bohari Baizura, Borlon Quentin, Bronz Murat, Proceedings of the Institution of Mechanical Engineers . 2020,第10期

机译：分布式推进器飞机概念的螺旋桨翼交互空气动力学模型
4. Aerodynamic Study of a Pusher-Propeller effects on a simple flap [C] . Algozino Santiago, Maranon Di Leo Julio, Delnero Juan Sebastian, AIAA applied aerodynamics conference;AIAA aviation forum . 2016

机译：简单推进器襟翼上推进器-螺旋桨效应的空气动力学研究
5. Experimental Investigations on the Aerodynamic and Aeroacoustic Characteristics of Small UAS Propellers [D] . Ning, Zhe. 2018

机译：小型UAS螺旋桨空气动力学和空气声学特性的实验研究。
6. Multi-Objective Aerodynamic Optimization of the Streamlined Shape of High-Speed Trains Based on the Kriging Model [O] . Gang Xu, Xifeng Liang, Shuanbao Yao, -1

机译：基于克里格模型的高速列车流线型多目标气动优化
7. Aerodynamic characteristics of a propeller-powered high-lift semispan wing [O] . Applin Zachary T., Takallu M. A., Gentry Garl L. Jr. 1994

机译：螺旋桨驱动的高升力半跨机翼的空气动力学特性

Aerodynamic characteristics of a 1/8-scale powered model of a high-speed bomber with a dual pusher propeller aft of the empennage

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