Aerodynamic data for the BAC 221 up to a mach number of 0.955 as measured in wind tunnel tests

Aerodynamic data for the BAC 221 up to a mach number of 0.955 as measured in wind tunnel tests

Dorothy M. Holford
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/1243
Date: 1972

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