Wind tunnel tests and flight tests on a business aircraft are compared. The direct method involves comparing the unitary curves obtained from the two tests, whereas the indirect method consists of establishing from the wind tunnel tests a basic set of adjusted parameters that are converted into the same time based parameters recorded on flight test tapes, using flight mechanics equations and a simulation program. Results of longitudinal and lateral tests are discussed. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Comparison of Wind Tunnel Tests and Flight Tests on an Executive Aircraft


    Erscheinungsdatum :

    1976


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch