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Investigation of effect of sideslip on lateral stability characteristics III : rectangular low wing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface

机译：侧滑对侧向稳定性影响的研究III：圆形机身上的矩形低翼，垂直尾翼面积和机身长度随水平尾翼的变化而变化

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作者
Hollingworth, Thomas A;
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年度 1945
页码 1-20
总页数 20
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
SIDESLIPPING; STABILITY & CONTROL, LATERAL; TAIL SURFACES, VERTICAL; TAIL SURFACES, HORIZONTAL; FUSELAGES, CIRCULAR; MONOPLANES, LOW-WING; FUSELAGE-WING COMBINATIONS; TAIL SURFACES - AREA; WINGS - DIHEDRAL; AIRFOILS - NACA 23012;

机译：侧滑;稳定性和控制，横向; TaIL sURFaCEs，VERTICaL; TaIL sURFaCEs，HORIZONTaL; FUsELaGEs，CIRCULaR; mONOpLaNEs，LOW-WING; FUsELaGE-WING组合; TaIL sURFaCEs - aREa; WINGs - DIHEDRaL; aIRFOILs - NaCa 23012;

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1. 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

机译：关于翼空气动力学预测及其对水平尾部的影响的风洞壁效应和机翼机身干扰
2. Computational analysis of static height stability and aerodynamics of vehicles with a fuselage, wing and tail in ground effect [J] . Lee Juhee Ocean Engineering . 2018,第NOVa15期

机译：具有地面，机翼和机尾的车辆的静态高度稳定性和空气动力学的计算分析
3. Characteristics of Liquid Film Flowing around Side Wall of a Horizontal Circular Cylinder (Wave Length of Standing Wave Appearing on Film Surface) [J] . Kenji KATOH, Tsuneo AZUMA 日本機械学会論文集. B編 . 2000,第643期

机译：液膜绕水平圆柱体侧壁流动的特性（在膜表面上出现驻波的波长）
4. OPTIMISATION OF A WING-BODY-TAIL CONFIGURATION WITH AN ALTERNATIVE LOW DRAG FUSELAGE AND BODY TRAILING EDGE [C] . Smith L., Craig K.J., Meyer J.P., Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：低尾翼机身和机车尾缘优化机翼尾翼构型
5. Wind tunnel tests on the effect of power on the stability of a low wing monoplane with three vertical positions of horizontal tail surfaces [O] . Bolster Calvin Mathews 1936

机译：风洞试验功率对水平尾翼三个垂直位置的低翼单翼飞机稳定性的影响
6. INVESTIGATION OF EFFECT OF SIDESLIP ON LATERAL STABILITY CHARACTERISTICS III - RECTANGULAR LOW WING ON CIRCULAR FUSELAGE WITH VARIATIONS IN VERTICAL-TAIL AREA AND FUSELAGE LENGTH WITH AND WITHOUT HORIZONTAL TAIL SURFACE [R] . Thomas A. Hollingworth 1945

机译：sIDEsLIp对横向稳定性特征的影响研究III - 矩形低翼对垂直尾部区域的变化和具有和没有水平尾部表面的固化长度的影响

Investigation of effect of sideslip on lateral stability characteristics III : rectangular low wing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface

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