Methodology is developed and described for estimating the flight performance and weights of a helicopter for which limited data are available. The methodology is based on assumptions which couple knowledge of the technology of the helicopter under study with detailed data from well documented helicopters thought to be of similar technology. The approach, analysis assumptions, technology modeling, and the use of reference helicopter data are discussed. Application of the methodology is illustrated with an investigation of the Agusta A129 Mangusta.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Methodology for estimating helicopter performance and weights using limited data


    Beteiligte:
    Baserga, Claudio (Autor:in) / Ingalls, Charles (Autor:in) / Lee, Henry (Autor:in) / Peyran, Richard (Autor:in)

    Kongress:

    Vertical Lift Aircraft Design Conference ; 1990 ; San Francisco, CA, United States


    Erscheinungsdatum :

    1990-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Method of estimating helicopter performance

    Payne, P.R. | Engineering Index Backfile | 1953


    Limited Performance Tests CH-54B (Tarhe) Helicopter

    J. N. Johnson / V. L. Diekmann / J. M. Johnson et al. | NTIS | 1973


    A Method of Estimating Helicopter Performance

    Payne, P.R. | Emerald Group Publishing | 1953


    Estimating Aircraft Landing Weights from Mode S Data

    Holzäpfel, Frank N. / Rotshteyn, Grigory | AIAA | 2022


    Estimating Aircraft Landing Weights from Mode S Data

    Holzäpfel, Frank / Rotshteyn, Grigory | Deutsches Zentrum für Luft- und Raumfahrt (DLR) | 2022

    Freier Zugriff