Methods to analyze the aerodynamic performance of V/STOL inlets at the NASA Lewis Research Center are discussed with emphasis on recent extensions and applications. Methods include the specification of the Kutta condition for a slotted inlet, the calculation of suction and tangential blowing for boundary layer control, and the analysis of auxiliary inlet geometries at angles of attack. An optimum diffuser velocity distribution is also developed, which can result in the shortest no-boundary layer control inlet and the lowest loss for the required amount of diffusion.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A summary of V/STOL inlet analysis methods


    Beteiligte:
    Hwang, D. P. (Autor:in) / Diedrich, J. H. (Autor:in)

    Kongress:

    V/STOL Conference ; 1981 ; Palo Alto, CA


    Erscheinungsdatum :

    01.12.1981


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    A summary of V/STOL inlet analysis methods

    Hwang, D. P. / Abbott, J. M. | NTRS | 1982


    A Summary of V/STOL Inlet Analysis Methods

    D. P. Hwang / J. M. Abbott | NTIS | 1982




    A summary of V/STOL inlet analysis methods

    HWANG, D. / DIEDRICH, J. | AIAA | 1981