Contents: Transonic Wing and Far Field Test Data on a High Aspect Ratio Transport Wing for Three Dimensional Computational Method Evaluation; Transonic Wing and Far Field Test Data on a Moderate Aspect Ratio Wing for Three Dimensional Computational Method Evaluation; Pressure Distributions Measured on Research Wing M100 Mounted on an Axisymmetric Body; Pressure Distribution Measured on Research Wing M86 Mounted on an Axisymmetric Body; and Pressure Distribution on a Swept Wing Aircraft in Flight.


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    Titel :

    Experimental Data Base for Computers Program Assessment. Addendum. Report of the Fluid Dynamics Panel Working Group 04


    Erscheinungsdatum :

    1984


    Format / Umfang :

    154 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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