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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    Title :

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


    Contributors:

    Publication date :

    1975


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English