NASA Technical Reports Server (NASA) · 1976 · 12 citations · 0 references
EngineeringAerospace EngineeringComputational EngineeringAerodynamicsAircraft DesignComputational MechanicsAerodynamic DesignAircraft Configuration DesignComputational AerodynamicsFlight SimulationSupersonic AerodynamicsWing AerodynamicsAerodynamic Force GenerationAerodynamic Force ModelingAerodynamic LoadingAerodynamic LoadsAerodynamic ModelingAircraft Aerodynamic DesignLinear Aerodynamic ModelingSupersonic Aircraft Configuration
An integrated system of computer programs was developed for the design and analysis of supersonic configurations. 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 are optional at the user's request. This user's manual contains a description of the system, an explanation of its usage, the input definition, and example output.