REG NACA-TN-2941-1953
The drag of finite-length cylinders determined from flight tests at high Reynolds numbers for a Mach number range from 0.5 to 1.3
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REG NACA-TN-2941-1953
Standard No.
REG NACA-TN-2941-1953
Release Date
1953
Published By
GB-REG
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