Authors: Langley Aeronautical Laboratory

  • Wind-tunnel Investigation of a Rectangular NACA 2212 Airfoil With Semispan Ailerons and With Nonperforated, Balanced Double Split Flaps for Use as Aer — Langley Aeronautical Laboratory

    Wind-tunnel Investigation of a Rectangular NACA 2212 Airfoil With Semispan Ailerons and With Nonperforated, Balanced Double Split Flaps for Use as Aer — Langley Aeronautical Laboratory

  • Wind-tunnel Investigation of Control-surface Characteristics.: XXIII, a 0.25-airfoil-chord Flap With Tab Having a Chord Twice the Flap Chord on an NAC — Langley Aeronautical Laboratory

    Wind-tunnel Investigation of Control-surface Characteristics.: XXIII, a 0.25-airfoil-chord Flap With Tab Having a Chord Twice the Flap Chord on an NAC — Langley Aeronautical Laboratory

  • Theory of Propellers III, the Slipstream Contraction with Numerical Values for Two-Blade and Four-blade Propellers — Langley Aeronautical Laboratory

    Theory of Propellers III, the Slipstream Contraction with Numerical Values for Two-Blade and Four-blade Propellers — Langley Aeronautical Laboratory

  • Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel — Langley Aeronautical Laboratory

    Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel — Langley Aeronautical Laboratory

  • Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel — Langley Aeronautical Laboratory

    Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel — Langley Aeronautical Laboratory