NASA NACA-RM-A54F18-1954由美国宇航局 US-NASA 发布于 1954-01-01。NASA NACA-RM-A54F18-1954 当马赫数达到0.94时,有NACA4个数字或NACA64A厚度分布的后掠机翼的纵向空气动力特性对比的最新版本是哪一版?NASA NACA-RM-A54F18-1954已经是当前最新版本。标准...
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...
NACA 64A 010Les motivations profondes de ces recherches trouvent leurs origines dans la connaissance et la determination des caracteristiques aerodynamiques des ailes aux differents angles d'incidences numeriquement et experimentalement, et dans leurs applications a un tres grand nombre de problemes ...
纳卡-64A.203-翼型-1(naca-64a203-airfoil-1) 作品集:3D模型5834套 唯_344 5个月前 纳卡0015 翼型(NACA0015 airfoil) 作品集:3D模型_G388284套 James_Walker 4个月前 翼型宏_NACA翼型_(Airfoil macros _NACA airfoil_) 作品集:3D模型_G388284套 ...
NACA 0010-34 Preview Details NACA 0010-64 Preview Details NACA 64A-010 10.0% Preview DetailsPolars for NACA 63A010 AIRFOIL (n63010a-il)PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource n63010a-il 50,000 9 27.3 at α=4.5° Mach=0 Ncrit=9 Xfoil prediction Details n63010a-il 50,000 5 ...
我手上有一个小软件，叫naca aerofoil sections，可以导出想要的naca翼型坐标值。在网上搜搜看，应该能...
SW9#traceroute mac 001a.64a3.ffcb 0080.9174.f201 Source 001a.64a3.ffcb found on SW6 1 SW6 (172.31.100.16) : Fa0/3 => Gi0/2 2 SW7 (172.31.100.17) : Gi0/1 => Gi0/2 3 SW8 (172.31.100.18) : Gi0/1 => Gi0/2 4 SW9 (172.31.100.19) : Gi0/1 => Fa0/11 Destination ...
SW9#traceroute mac 001a.64a3.ffcb 0080.9174.f201 Source 001a.64a3.ffcb found on SW6 1 SW6 (172.31.100.16) : Fa0/3 => Gi0/2 2 SW7 (172.31.100.17) : Gi0/1 => Gi0/2 3 SW8 (172.31.100.18) : Gi0/1 => Gi0/2 4 SW9 (172.31.100.19) : Gi0/1 => Fa0/11 Destination ...
纳卡-64A.203-翼型-1(naca-64a203-airfoil-1) 作品集:3D模型100套 唯_344 5个月前 纳卡0015 翼型(NACA0015 airfoil) 作品集:3D模型_G100套 James_Walker 3个月前 纳卡2212 翼型(naca 2212 airfoil) 作品集:3D模型_G100套 James_Walker 2个月前 ...
NASA NACA-RM-A54F18-1954的引用关系信息,当马赫数达到0.94时,有NACA4个数字或NACA64A厚度分布的后掠机翼的纵向空气动力特性对比, A comparison of the longitudinal aerodynamic characteristics at mach numbers