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    Correlation of Predicted and Measured Thermal Stresses on a Truss-Type Aircraft Structure

    Correlation of Predicted and Measured Thermal Stresses on a Truss-Type Aircraft Structure


    A test structure representing a portion of a hypersonic vehicle was instrumented with strain gages and thermocouples. This test structure was then subjected to laboratory heating representative of supersonic and hypersonic flight conditions. A finite element computer model of this structure was developed using several types of elements with the NASA structural analysis (NASTRAN) computer program. Temperature inputs from the test were used to generate predicted model thermal stresses and these were correlated with the test measurements.

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    Titel :

    Correlation of Predicted and Measured Thermal Stresses on a Truss-Type Aircraft Structure

    Beteiligte:
    J. M. Jenkins (Autor:in) / L. S. Schuster (Autor:in) / A. L. Carter (Autor:in)
    Erscheinungsdatum :

    1978

    Format / Umfang :

    57 pages

    Medientyp :

    Report

    Format :

    Keine Angabe

    Sprache :

    Englisch

    Schlagwörter :

    Manned Spacecraft , Hypersonic vehicles , Thermal stresses , Computerized simulation , Nastran , Data correlation , Heat transfer , Prediction analysis techniques , Temperature measurement

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