This is the presentation to follow conference paper of the same name. The adaptive compliant trailing edge (ACTE) flap experiment safety of flight requires that the flap to wing interface loads be sensed and monitored in real time to ensure that the wing structural load limits are not exceeded. This paper discusses the strain gage load calibration testing and load equation derivation methodology for the ACTE interface fittings. Both the left and right wing flap interfaces will be monitored and each contains four uniquely designed and instrumented flap interface fittings. The interface hardware design and instrumentation layout are discussed. Twenty one applied test load cases were developed using the predicted in-flight loads for the ACTE experiment.


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    Titel :

    Strain Gage Load Calibration of the Wing Interface Fittings for the Adaptive Compliant Trailing Edge Flap Flight Test


    Beteiligte:
    Miller, Eric J. (Autor:in) / Holguin, Andrew C. (Autor:in) / Cruz, Josue (Autor:in) / Lokos, William A. (Autor:in)

    Kongress:

    AIAA SciTech Conference ; 2014 ; National Harbor, MD, United States


    Erscheinungsdatum :

    2014-01-13


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Strain Gage Load Calibration of the Wing Interface Fittings for the Adaptive Compliant Trailing Edge Flap Flight Test (AIAA 2014-0277)

    Miller, E.J. / Holguin, A.C. / Cruz, J. et al. | British Library Conference Proceedings | 2014



    Approach for Structurally Clearing an Adaptive Compliant Trailing Edge Flap for Flight

    Miller, Eric J. / Lokos, William A. / Cruz, Josue et al. | NTRS | 2015


    Approach for Structurally Clearing an Adaptive Compliant Trailing Edge Flap for Flight

    Miller, Eric J. / Lokos, William A. / Cruz, Josue et al. | NTRS | 2015