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Investigation of effects of various camouflage paints and painting procedures on the drag characteristics of an NACA 65(sub 421)-420, a = 1.0 airfoil section

机译：研究各种迷彩涂料和涂装工艺对NaCa 65（sub 421）-420，a = 1.0翼型截面阻力特性的影响

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作者
Braslow, Albert L;
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年度 1944
页码 1-10
总页数 10
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIRFOILS - NACA 65 (421)-4220-CHARACTERISTICS LOW-DRAG; PAINTS, CAMOUFLAGE; REYNOLDS NUMBER; LIFT COEFFICIENTS - AIRFOILS - NACA 65 (421)-420; DRAG - WINGS EFFECT OF PAINT; WIND TUNNEL TESTS - NACA - PRESSURE, TWO-DIMENSIONAL LMAL;

机译：aIRFOILs - NaCa 65（421）-4220-特征低拖; paINTs，CamOUFLaGE; REYNOLDs NUmBER;提升系数 - 翼型 - NaCa 65（421）-420; DRaG - 涂料的翅膀效果;风洞测试 - NaCa - 压力，二维LmaL;
入库时间 2022-08-29 11:20:30

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Investigation of effects of various camouflage paints and painting procedures on the drag characteristics of an NACA 65(sub 421)-420, a = 1.0 airfoil section

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