哪些标准引用了NASA NACA-TN-3007-1953 找不到引用NASA NACA-TN-3007-1953 装配有前缘板条,前缘襟翼,分裂式襟翼和双开缝襟翼的多种组合的NACA 64A010翼剖面的低速升力和倾斜力矩 的标准 标准号 NASA NACA-TN-3007-1953 发布 1953年 总页数 46页 发布单位 美国宇航局 购买 正式版...
Airfoil: NACA 64A-010 10.0% (naca64a010-il)Reynolds number: 50,000Max Cl/Cd: 26.58 at α=4.25°Description: Mach=0 Ncrit=9Source: Xfoil predictionDownload polar: xf-naca64a010-il-50000.txtDownload as CSV file: xf-naca64a010-il-50000.csv XFOIL Version 6.96 Calculated polar for: NACA 64...
NASA NACA-TN-3007-1953 装配有前缘板条,前缘襟翼,分裂式襟翼和双开缝襟翼的多种组合的NACA 64A010翼剖面的低速升力和倾斜力矩 NASA NACA-WR-L-301-1941 操纵面特性II的风洞研究.和NACA 0009机翼上30%弦襟翼一起使用的多种机头形状小空气动力天平 NASA NACA-TN-1293-1947 带有板条和双开缝襟翼和抽吸边界层控制...
Braslow, Albert LLangley Research CenterVisconti, FioravanteBraslow, A., Visconti, F.: Further experimental studies of area suction for the control of the laminar boundary layer on a porous bronze NACA 64A010 airfoil. NACA Technical Note 2112, 1950....
HB/Z 321-1998 飞机增升装置设计指南HB/Z 20013-2012 无人驾驶飞机气动布局设计指南NASA NACA-TN-3007-1953 装配有前缘板条,前缘襟翼,分裂式襟翼和双开缝襟翼的多种组合的NACA64A010翼剖面的低速升力和倾斜力矩NASA NACA-ACR-L4D12-1944 对操纵面特性17的风洞研究.NACA0009机翼上0.20,0.30和0.40翼弦的倾斜机翼后...
Two-Dimensional Wind-Tunnel Tests of a Jet-Type Spoiler on an Naca 64A010 Airfoil Section Equipped with High-Lift Devices.AirfoilsJetsSpoilersAerodynamic characteristicsModel testsWind tunnel modelsNo abstract available.Ballentine, D. CDavid Taylor Model BasinBarnard, G. A...
HB/Z 321-1998 飞机增升装置设计指南 HB/Z 20013-2012 无人驾驶飞机气动布局设计指南 NASA NACA-TN-3007-1953 装配有前缘板条,前缘襟翼,分裂式襟翼和双开缝襟翼的多种组合的NACA 64A010翼剖面的低速升力和倾斜力矩 GB/T 16638.3-2008 空气动力学 概念、量和符号.第3部分:飞机几何特性 NASA NACA-ACR-L4D12-...
Hemenover, A.D.: Tests of the NACA 64-010 and 64A010 airfoil sections at high subsonic Mach numbers. NACA-RM-A9E31. Moffett Field (1949)P.P. Polentz. Comparison of the aerodynamic characteristics of the NACA0010 and 0010-64 airfoil sections at high subsonic Mach numbers. RM A9G19, ...