A procedure has been established for the utilization of a computer to calculate coordinates of curves described by the second degree equation as used in defining the shape of aircraft components. Based on the same preliminary sketches and input data used in the graphical method of development, longitudinal basic lines and transverse contours can be quickly calculated to describe an entire three dimensional surface. The output data are utilized for currently established three dimensional mock-up techniques and hardware design.The paper presents the mathematical background and a complete explanation of the procedure used to develop a three dimensional surface. Design optimization, hardware design, and utilization of supplementary information are discussed. Appendices include the general computer program and a sample design problem.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Computer Utilization for Aircraft Contour Determination


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    National Business Aircraft Meeting and Engineering Display ; 1970



    Erscheinungsdatum :

    1970-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Object contour determination

    CHEN YUANYUAN / WANG ZENG | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft Noise Source and Contour Estimation

    D. G. Dunn / N. A. Peart | NTIS | 1973


    OBJECT CONTOUR DETERMINATION

    CHEN YUANYUAN / WANG ZENG | Europäisches Patentamt | 2022

    Freier Zugriff

    Aircraft noise source and contour estimation

    Dunn, D. G. / Peart, N. A. | NTRS | 1973


    Comparison of aircraft noise-contour prediction programs

    CHAPKIS, R. / BLANKENSHIP, G. / MARSH, A. | AIAA | 1980