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Ph.D. Student, Pardee RAND Graduate School, and Assistant Policy Researcher, RAND
A 1953 RAND study that investigates the problem of prediction of airplane drag divergence Mach number and provides an empirically determined expression that is applicable to clean airplane configurations.
Aug 1, 1953
A study of the turbulent boundary-layer drag for production-type or nonideal aircraft surfaces.
Jun 24, 1953