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Large scale wind tunnel investigation of a semispan wing equipped with an externally-blown jet flap

机译：大型风洞调查半翼机翼配备外吹式喷射翼

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摘要

A wind tunnel investigation was made of the aerodynamic characteristics of a 14.5 foot semispan, externally-blown jet flap model. The model was equipped with a single 30-inch diameter, ducted fan with a 1.03 pressure ratio. The effects of flap size, fan vertical location, and wing sweep on the longitudinal aerodynamic characteristics were studied.

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作者
Falarski, M. D.; Aiken, T. N.;
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年度 1971
页码 1-97
总页数 97
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; JET FLAPS; SEMISPAN MODELS; WIND TUNNEL MODELS; AERODYNAMIC CONFIGURATIONS; DUCTED FANS; SWEPT WINGS;

机译：空气动力学特征; JET FLaps; sEmIspaN模型;风洞模型;空气动力学配置; DUCTED FaNs; sWEpT WINGs;

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1. Two Optical Techniques Appropriate for Visualizing the Steady／Unsteady Vortical Flow Past a Highly Swept Delta—Wing Equipped with Double Vortex—Flaps in Low and High Speed Wind—Tunnel [J] . GongNI, DingdingXIN, 等非线性科学与数值模拟通讯：英文版 . 1998,第003期

机译：两种可视化技术，适用于可视化经过高掠过三角洲的稳定/不稳定涡流-配备双涡旋的机翼-在低速和高速风洞中的襟翼
2. Wind Tunnel Investigation of a Circulation Control Wing with Dual-Radius Flaps [J] . Kanistras Konstantinos, Saka Pranith Chander, Valavanis Kimon P., Journal of Aircraft . 2018,第4期

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3. Investigation of wind tunnel wall effect and wing-fuselage interference regarding the prediction of wing aerodynamics and its influence on the horizontal tail [J] . Hoang Ngoc T. B., Bui Binh V. Journal of Mechanical Science and Technology . 2019,第6期

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4. Real-Time Adaptive Drag Minimization Wind Tunnel Investigation of a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System [C] . Nhan Nguyen, Nicholas Cramer, Kelley Hashemi, AIAA aviation forum . 2019

机译：可变弯度连续后缘襟翼系统的柔性机翼实时自适应风阻最小化风洞研究
5. Wind tunnel test of a tailless aircraft with a belly-flap control surface used in combination with wing flaps. [D] . Dougherty, Daniel A. 2012

机译：带有襟翼控制面并与机翼襟翼配合使用的无尾飞机的风洞测试。
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. An Investigation into Scale Open Jet Wind Tunnel Corrections through the use of CFD and Wind Tunnel Testing [O] . Jordan T. 2014

机译：通过CFD和风洞测试对比例尺露天喷气式风洞校正的研究
8. Large Scale Wind Tunnel Investigation of a Semispan Wing Equipped with an Externally-Blown Jet Flap [R] . Falarski, M. D., Aiken, T. N. 1971

机译：三翼机翼的大型风洞调查，配备外部喷射式襟翼

Large scale wind tunnel investigation of a semispan wing equipped with an externally-blown jet flap

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