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Low speed wind tunnel investigation of a semispan STOL jet transport wing with deflected thrust and blowing boundary layer control

机译：半导体sTOL喷气运输机翼的低速风洞调查，具有偏转推力和吹动边界层控制

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摘要

Wind tunnel investigation of static longitudinal aerodynamic characteristics of semispan swept wing for STOL jet transport with deflected thrust and boundary layer control

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作者
Henderson, R. L.;
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年度 1971
页码 1-87
总页数 87
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; SHORT TAKEOFF AIRCRAFT; TRANSPORT AIRCRAFT; AIRCRAFT STABILITY; BOUNDARY LAYER CONTROL; SWEPT WINGS;

机译：空气动力学特征;短途飞机;运输飞机;飞机稳定性;边界层控制; sWEpT WINGs;

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1. Research on Distributed Jet Blowing Wing Based on the Principle of Fan-Wing Vortex-Induced Lift and Thrust [J] . Du Siliang, Zhao Qijun, Wang Bo International journal of aerospace engineering . 2019,第PTa3期

机译：基于风扇翼涡流诱导升力和推力原理分布式喷射吹翼的研究
2. Research on Distributed Jet Blowing Wing Based on the Principle of Fan-Wing Vortex-Induced Lift and Thrust [J] . Du Siliang, Zhao Qijun, Wang Bo International journal of aerospace engineering . 2019,第4期

机译：基于风扇翼涡流诱导升力和推力原理分布式喷射吹翼的研究
3. Blowing jets as a circulation flow control to enhancement the lift of wing or generated power of wind turbine [J] . Alexandru DUMITRACHE, Florin FRUNZULICA, Horia DUMITRESCU, INCAS Bulletin . 2014,第2期

机译：吹气喷嘴作为循环流量控制，可增强机翼的升力或风力发电机的发电功率
4. BOUNDARY-LAYER CONTROL BY BLOWING AT THE TEST-SECTION OF A LOW-SPEED WIND TUNNEL [C] . Marcelo Assato, Nide G C R Fieo Jr, Roberto M Girardi Congress of the International Council of the Aeronautical Sciences . 2006

机译：低速风隧道试验段吹出边界层控制
5. Characterization of a low-speed boundary layer wind tunnel. [D] . Hauptman, Zachary. 2010

机译：低速边界层风洞的特征。
6. Aerodynamic evaluation of wing shape and wing orientation in four butterfly species using numerical simulations and a low-speed wind tunnel and its implications for the design of flying micro-robots [O] . Alejandro Ortega Ancel, Rodney Eastwood, Daniel Vogt, 2017

机译：利用数值模拟和低速风洞对四种蝶类的翼形和翼向进行空气动力学评估及其对飞行微型机器人设计的启示
7. Further low speed wind tunnel tests on slender cambered wings with apex blowing. [O] . Cole Joseph D. 1968

机译：在带有尖顶吹气的细长弧形机翼上进行进一步的低速风洞测试。
8. Low Speed Wind Tunnel Investigation of a Semispan STOL Jet Transport Wing with Deflected Thrust and Blowing Boundary Layer Control [R] . Henderson, R. L. 1971

机译：具有偏转推力和吹动边界层控制的半跨sTOL喷射输送机翼的低速风洞研究

Low speed wind tunnel investigation of a semispan STOL jet transport wing with deflected thrust and blowing boundary layer control

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