Computation of 3-D transonic flows for wings and wing body configuration, annual progress report

Chakrabartty, SK and Subramanian, NR (1986) Computation of 3-D transonic flows for wings and wing body configuration, annual progress report. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    The object of the present work was to validate the two well known codes STWING and SFL022 to compute the transonic flow past. wings. The results obtained by these codes for OKBRA-M6 and Rectangular wings have been presented. The agreements among these two codes and available experimental results are satisfactory.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Transonic flows wings
    Subjects: AERONAUTICS > Aeronautics (General)
    Division/Department: Flight Mechanics and Control Division, Flight Mechanics and Control Division
    Depositing User: Poornima Narayana
    Date Deposited: 03 Aug 2006
    Last Modified: 24 May 2010 09:46
    URI: http://nal-ir.nal.res.in/id/eprint/2235

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