Aerodynamic coefficients are presented for perfect-gas and equilibrium-air solutions of the Navier-Stokes equations about the Stardust reentry-capsule forebody at Mach numbers of 4.6, 7, 8.5, and 10. A comparison with Newtonian-flow assumptions indicates a divergence of the aerodynamic coefficients from Newtonian-flow for Mach numbers less than 10. The static stability of the forebody is reduced by a factor of 2.5 with decreasing freestream Mach number between Mach 10 and 7.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hypersonic Pitching-Moment Shift for Stardust Reentry Capsule Forebody


    Beteiligte:
    W. A. Wood (Autor:in)

    Erscheinungsdatum :

    1997


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Post-Flight Evaluation of Stardust Sample Return Capsule Forebody Heatshield Material

    Stackpoole, Mairead / Sepka, Steve / Cozmuta, Ioana et al. | AIAA | 2008


    Post-Flight Evaluation of Stardust Sample Return Capsule Forebody Heatshield Material

    Stackpoole, M. / Sepka, S. / Cozmuta, I. et al. | British Library Conference Proceedings | 2008


    Imaging and Slitless Spectroscopy of the Stardust Capsule Reentry Radiation

    Harms, Franziska / Wolf, Juergen / Raiche, George et al. | AIAA | 2010



    Forebody TPS sizing with radiation and ablation for the Stardust Sample Return Capsule

    Olynick, Dave / Chen, Y.-K. / Tauber, Michael | AIAA | 1997