20 research outputs found

    A system for aerodynamic design and analysis of supersonic aircraft. Part 3: Computer program description

    Get PDF
    The computer program documentation for the design and analysis of supersonic configurations is presented. Schematics and block diagrams of the major program structure, together with subroutine descriptions for each module are included

    A computational system for aerodynamic design and analysis of supersonic aircraft. Part 2: User's manual

    Get PDF
    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

    Aerodynamic design and analysis system for supersonic aircraft. Part 2: User's manual

    Get PDF
    An integrated system of computer programs for supersonic configurations is described. An explanation of system usage, the input definitions, and example output are included. For Part 1, see N75-18185; for Part 3, see N75-18186

    Computational transonic analysis of canted winglets

    Full text link
    corecore