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  • Cl v Alpha nasasc2-0714-il Re50000
    AlinaNeh Airfoil database N-list
    aircraftairplaneairfoilswingsstabilizers
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  • Cl v Alpha isa571-il Re50000
    AlinaNeh Airfoil database I-list
    aircraftairplaneairfoilswingsstabilizers
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  • Lift coefficient (Angle of Attack) - experiment
    nomad-vagabond Wind turbine airfoil catalogue
    lift coefficientdrag coefficientaerodynamicsnacaairfiolwind turbineairbladeairfoilsdeg. : 1
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  • Max Force vs Diameter
    Serhii.K Quadcopter Frame Design Parameters
    framedronequadcopterstifness
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  • Thrust vs Throttle
    Serhii.K Alva Industries X60 Electric Motor
    coptermotorsmulticopterbrushlesselectricdroneµs : g
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  • PMMA+LOX: c*(O/F)
    scorpaena Hybrid Rocket Propellants
    propellantimpulseoxidanttemperature
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  • CCl*c/cref by span (Gamma=12 AR=6 AoA=0)
    nomad-vagabond Swept wing vorticity analysis
    lift coefficientaerodynamicswing
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  • CL vs alpha
    nomad-vagabond Test
    aerodynamics
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  • Deformation (ANSYS) vs Length
    Serhii.K Rectangular Beam Bending Analyses
    beambendingansyslongeronefemdeformation
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  • Isp(ROF) Pe = 1 kPa
    scorpaena Data for Ethanol and Kerosene Propellant for Gas-Generator Fed Upper Stage Application
    ecosimproethanolcycle analysisgas generatorliquid rocket enginerocket engine1 : m/s
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