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Pressure distribution over a plug-type spoiler-slot aileron on a tapered wing with full span slotted flaps

机译：压力分布在锥形机翼上的插头式扰流板 - 副翼副翼上，带有全跨度开槽襟翼

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作者
Lowry, John G; Turner, Thomas R;
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年度 1946
页码 1-31
总页数 31
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIRFOILS - NACA 230 - CHAR , MOMENTS & ORDINATES WING FLAPS, SLOTTED & AILERONS,; AIRPLANES, FIGHTER; FLYING, HIGH-SPEED; LOADS-AILERONS; PRESSURE DISTRIBUTION-AILERONS, SPOILER-SLOT (PLUG); WING FLAPS, SLOTTED & AILERONS, SPOILER-SLOT (PLUG); WINGS, TAPERED - CHARACTERISTICS EFFECT OF WING FLAPS; AIRPLANES - GRUMMAN F4F-3 - WIND TUNNEL TESTS (NACA-7'X 10') (AMER );

机译：aIRFOILs - NaCa 230 - CHaR，mOmENTs＆amp; ORDINaTEs WING FLaps，sLOTTED＆amp;副翼，; aIRpLaNEs，FIGHTER;飞行，高速;载荷，副翼;压力分布 - aILERONs，spOILER-sLOT（pLUG）; WING FLaps，sLOTTED＆amp; aILERONs，spOILER-sLOT（pLUG）; WINGs，TapERED - 翼片的特征效应;飞机 - GRUmmaN F4F-3 - 风洞测试（NaCa-7'X 10'）（美国）;

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1. Unsteady pressure distribution of a flapping wing undergoing root flapping motion with elbow joint at different reduced frequencies [J] . Razaami A. F., Zorkipli M. K.H.M., Lai H. C., International Review of Aerospace Engineering . 2017,第3期

机译：襟翼根部拍打运动在不同减小频率下的拍打翼的非定常压力分布
2. Wing component allocation for a morphing variable span of tapered wing using finite element method and topology optimisation - application to the UAS-S4 [J] . Elelwi M., Calvet T., Botez R. M., The Aeronautical Journal . 2021,第1290期

机译：使用有限元方法和拓扑优化的锥形机翼变形变形跨度的机翼组分分配 - 应用于UAS-S4
3. Study the Influence of a Gap between the Wing and Slotted Flap over the Aerodynamic Characteristics of Ultra-Light Aircraft Wing Airfoil [J] . Cvetelina Velkova, Michael Todorov, Guillaume Durand 机械工程与自动化：英文版 . 2015,第005期

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4. Calculation Method for Optimal Circulation Distribution on a Finite Span Flapping Wing [C] . M. Harada AIAA's 1st Technical Conference and Workshop on Unmanned Aerospace Vehicles, Systems, Technologies, and Operations . 2002

机译：有限跨度扑翼上最佳环流分布的计算方法
5. THEORETICAL DETERMINATION OF THE PRESSURE DISTRIBUTION ON A LIFTING, SUBSONIC DELTA WING OF ARBITRARY ASPECT RATIO. [D] . SWAIN, CARL EUGENE. 1971

机译：从理论上确定任意纵横比的提升亚音速三角翼上的压力分布。
6. Multi-cored vortices support function of slotted wing tips of birds in gliding and flapping flight [O] . Marco KleinHeerenbrink, L. Christoffer Johansson, Anders Hedenström 2017

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7. In-flight non-intrusive measurement of wing dynamics and of the aileron and flap deflection and deformation [O] . Jentink H.W., Ružicka P., Veerman H.P.J., 2015

机译：机翼动力学，副翼和襟翼偏转和变形的飞行中非侵入式测量

Pressure distribution over a plug-type spoiler-slot aileron on a tapered wing with full span slotted flaps

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