Following a summary of the methods used to establish aerodynamic data and propulsion data, a comparison was made in the form of the drag (or thrust) difference between flight results and predictions made on the basis of these data. Certain hypothesis and improvements on aerodynamic data were presented in order to explain the slight deficit found on Airbus and Concorde.


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    Title :

    A comparison of predictions obtained from wind tunnel tests and the results from cruising flight: Airbus and Concorde


    Contributors:
    Berger, J. (author)

    Conference:

    Flight Mechanics Panel Specialists Meeting on Performance Prediction Methods ; 1977 ; Paris, France


    Publication date :

    1979-08-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English