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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Wind tunnel/flight data correlation for the Boeing 737-100 transport airplane


    Contributors:

    Publication date :

    1975-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English