A correlation of the forebody drag of cylinders with plane and hemispherical noses at mach numbers from zero to 2.5

A correlation of the forebody drag of cylinders with plane and hemispherical noses at mach numbers from zero to 2.5

A. Stanbrook
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/722
Date: 1964

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