A brief wind-tunnel/flight data correlation for the Boeing 737-100 airplane was made. The results showed excellent agreement between wind-tunnel and flight trimmed drag polars at Mach numbers less than 0.67. The wind-tunnel data predicted larger drag increments due to compressibility and a lift-curve slope about 9 percent higher than flight. (Author)


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    Titel :

    Wind Tunnel/Flight Data Correlation for the Boeing 737-100 Transport Airplane


    Beteiligte:
    F. J. Capone (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch








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