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Some lessons from NACA/NASA aerodynamic studies following World War II
Some comparisons of US and USSR aircraft design developments
Historical trend in the research and development of aircraft
Historical development of worldwide supersonic aircraft
Effects of body shape on the aerodynamics of a body of revolution at Mach numbers from 1.6 to 4.6
An overview of the potential threat as related to missile requirements
Aircraft research and development trends in the US and USSR