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Book
Significance of the expression CL³/CD²
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Year: 1924 Publisher: [Washington, D.C.] : National Advisory Committee for Aeronautics,

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Book
Significance of the expression CL³/CD²
Authors: ---
Year: 1924 Publisher: [Washington, D.C.] : National Advisory Committee for Aeronautics,

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Book
Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds
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Year: 1955 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 180°
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Year: 1955 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Book
Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 180°
Authors: --- --- ---
Year: 1955 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Book
Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds
Authors: --- ---
Year: 1955 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Book
Design guide for aerodynamics testing of Earth and planetary entry vehicles in a ballistic range
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Year: 2017 Publisher: [Moffett Field, California] : National Aeronautics and Space Administration, [Ames Research Cente]r,

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The aerodynamic characteristics of airfoils at negative angles of attack
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Year: 1932 Publisher: [Washington, D.C.] : National Advisory Committee for Aeronautics,

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The N.A.C.A. recording tachometer and angle of attack recorder
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Year: 1923 Publisher: [Washington, D.C.] : National Advisory Committee for Aeronautics,

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Exploratory low-speed wind-tunnel study of concepts designed to improve aircraft stability and control at high angles of attack
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Year: 1985 Publisher: [Washington, D.C.] : [National Aeronautics and Space Administration],

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