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Investigation of a 0.3-scale jet-transport model having a jet-augmented boundary-layer- control flap with direct-lift control capability

机译：研究具有直接升力控制能力的喷射增强边界层控制襟翼的0.3级喷射输送模型

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摘要

Trailing-edge flap system with boundary layer control and external jet augmentation for subsonic jet transport

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作者
Aoyagi, K.; Dickinson, S. O.; Soderman, P. T.;
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年度 1969
页码 1-86
总页数 86
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
BOUNDARY LAYER CONTROL; JET FLAPS; TRANSPORT AIRCRAFT; TRAILING EDGE FLAPS; AERODYNAMIC COEFFICIENTS; AIRCRAFT DESIGN; DRAG; GRAPHS (CHARTS); JET AIRCRAFT; WIND TUNNEL STABILITY TESTS; WING FLAPS;

机译：边界层控制; JET FLaps;运输飞机;拖尾边缘;空气动力学系数;飞机设计;拖动;图表（图表）;喷气式飞机;风洞稳定性试验;翼展;

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8. Investigation of a 0.3-Scale Jet-Transport Model Having a Jet-Augmented Boundary-Layer- Control Flap with Direct-Lift Control Capability [R] . Aoyagi, K., Dickinson, S. O., Soderman, P. T. 1969

机译：具有直接提升控制能力的具有喷射增强边界层控制襟翼的0.3级喷射传输模型的研究

Investigation of a 0.3-scale jet-transport model having a jet-augmented boundary-layer- control flap with direct-lift control capability

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