The Calculation of Pressure on Slender Airplanes in Subsonic and Supersonic Flow

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Report Number: NACA TN 2900
Author(s): Heaslet, Max A., Lomax, Harvard
Corporate Author(s): Ames Aeronautical Laboratory
Laboratory: National Advisory Committee for Aeronautics
Date of Publication: 1953-03
Pages: 29
DoD Task:
PB Number: PB108786
Identifier: AD0002873

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