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A system for aerodynamic design and analysis of supersonic aircraft. Part 2: User's manual
W. D. Middleton, J. L. Lundry, Roger G. Coleman
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Abstract
The system uses linearized theory methods for the calculation of surface pressures and supersonic area rule concepts in combination with linearized theory for calculation of aerodynamic force coefficients. Interactive graphics were included in the system to display or edit input and to permit monitoring and readout of program results.