NASA STI Repository (National Aeronautics and Space Administration) · 1980 · 23 citations · 10 references
Open access
EngineeringAerospace EngineeringMechanical EngineeringAerodynamicsAircraft DesignComputer-aided DesignAerodynamic DesignAircraft Configuration DesignAirfoil TheoryComputational AerodynamicsSupersonic AerodynamicsWing AerodynamicsAerodynamic Force GenerationAerodynamic Force ModelingAerodynamic LoadsAerodynamic ModelingAircraft Aerodynamic DesignAirfoil 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.
10