A flight test with a simplified HLFC system on the vertical tail plane of an A320 aircraft was performed in April/May 2018. In this paper we discuss the preparation of the flight test data for evaluation with linear stability theory on the basis of sample measurements. Then we present our correlated transition N-factors and compare them with the results of the A320 flight tests of 1998.


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    Title :

    Simplified Hybrid Laminar Flow Control for the A320 Fin Part 2: Evaluation with the e^N-method


    Contributors:

    Conference:

    2021 ; Virtuell


    Publication date :

    2021-01-15



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English