Theoretical wave drags and pressure distributions for axially symmetric open-nose bodies

John R. Jack
naca-tn-2115
Jun 1950


The variations of pressure distributions and coefficients of wave drag with fineness ratio, Mach number, and area ratio were calculated from linearized theory for a variety of open- nose bodies of revolution at zero angle of attack.

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http://naca.central.cranfield.ac.uk/reports/1950/naca-tn-2115.pdf