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Tests of the NACA 64(SUB 1)A212 airfoil section with a slat, a double slotted flap, and boundary-layer control by suction

机译：NaCa 64（sUB 1）a212翼型截面的测试，带有板条，双槽襟翼和抽吸边界层控制

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作者
Quinn, John H;
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年度 1947
页码 1-56
总页数 56
原文格式 PDF
正文语种 eng
中图分类工业技术 ;
关键词
AIRFOILS - NACA 641A212 - CHAR & ORDINATES LOW-DRAG (WING FLAPS,; SLOTTED (DOUBLE)); BOUNDARY LAYER CONTROL - SUCTION-SLOTS; WINGS - HIGH LIFT DEVICES; WING FLAPS, SLOTTED - DOUBLE; WING SLATS; REYNOLDS NUMBER; AIRFOIL SURFACES - ROUGHNESS; WIND TUNNEL TESTS - NACA - LOW-TURBULENCE (7 1/2'X 3') WORK CARRIED ON AT LMAL;

机译：aIRFOILs - NaCa 641a212 - CHaR＆amp; ORDINaTEs LOW-DRaG（WING FLaps; sLOTTED（DOUBLE））;边界层控制 - 抽吸槽; WINGs - 高升装置;翅膀，开口 - 双倍; WING sLaTs; REYNOLDs NUmBER;翼型表面 - 粗糙度;风洞测试 - NaCa - 低湍流（7 1 / 2'X 3'）工作在LmaL进行;

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8. Tests of the NACA 64 sub 1 A212 Airfoil Section with a Slat, a Double Slotted Flap, and Boundary-Layer Control by Suction [R] . Quinn, J. J. 1947

机译：的NaCa 64个子1 a212翼型截面与板条，一个双开缝折边，和边界层控制由吸试验

Tests of the NACA 64(SUB 1)A212 airfoil section with a slat, a double slotted flap, and boundary-layer control by suction

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