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Investigation of effect of sideslip on lateral stability characteristics II : rectangular midwing 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II：圆形机身上的矩形中翼，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 1-18
总页数 18
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; WINGS, RECTANGULAR; WINGS - DIHEDRAL; AIRFOILS - NACA 23012; FUSELAGE-WING COMBINATIONS; MONOPLANES, MID-WING;

机译：侧滑;稳定性和控制，横向; TaIL sURFaCEs，VERTICaL; TaIL sURFaCEs，HORIZONTaL; FUsELaGEs，CIRCULaR; WINGs，RECTaNGULaR; WINGs - DIHEDRaL; aIRFOILs - NaCa 23012; FUsELaGE-WING组合;中间地区;

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

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