Detailed numerical method for determining conformal mapping coefficients for complicated shapes is developed; body contour of each cross section is approximated by series of line segments and limited to singly connected regions; mapping process is readily adaptable to computer and has been programmed on IBM-7094; three cross sections, typical of re-entry vehicle shapes, mapped with good accuracy, are shown; aerodynamic derivatives and load distribution at low angles of attack are presented for re-entry vehicle, blunted 13° half-cone.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Conformal mapping method to predict low-speed aerodynamic characteristics of arbitrary slender re-entry shapes


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Skulsky, R.S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Continuous Aerodynamic Modelling of Entry Shapes

    Dirkx, Dominic / Mooij, Erwin | AIAA | 2011


    Continuous Aerodynamic Modelling of Entry Shapes

    Dirkx, D. / Mooij, E. / American Institute of Aeronautics and Astronautics; Conferderation of European Aerospace Societies | British Library Conference Proceedings | 2011


    Continuous Aerodynamic Modelling of Entry Shapes

    Dirkx, D. / Mooij, E. | British Library Conference Proceedings | 2011