Critical technologies are being developed to support the goals of the NASA Office of Aeronautics and Space Transportation Technology Access to Space initiative for next-generation reusable space transportation systems. From the perspective of aerothermodynamic performance throughout the flight trajectory, the Reusable Launch Vehicle program incorporates conceptual analysis, ground-based testing, and computational fluid dynamics to provide flyable suborbital flight demonstrator vehicles. This report provides an overview of the hypersonic aeroheating wind tunnel test program conducted at the NASA Langley Research Center in support of one of these vehicles, the X-34 small reusable technology demonstrator program. Global surface heat transfer images, surface streamline patterns, and shock shapes were measured on 0.0153- and 0.0183-scale models of proposed X-34 flight vehicles at Mach 6 and 10 in air. The primary parametrics that were investigated include angles-of-attack from 0 to 35 deg. and freestream unit Reynolds numbers from 0.5 to 8 million per foot (which was sufficient to produce laminar, transitional, and turbulent heating data), both with and without control surface deflections. Comparisons of the experimental data to computational predictions are included, along with a discussion of the implications of some of the experimental flow features for the flight vehicle.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    X-34 Experimental Aeroheating at Mach 6 and 10


    Beteiligte:

    Kongress:

    Aerospace Sciences Meeting and Exhibit ; 1998 ; Reno, NV, United States


    Erscheinungsdatum :

    1998-01-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    X-38 Experimental Aeroheating at Mach 10

    Berry, S.A. | Online Contents | 2004


    X-38 Experimental Aeroheating at Mach 10

    Scott Berry / Thomas Horvath / K. Weilmuenster et al. | AIAA | 2004


    X-38 Experimental Aeroheating at Mach 10

    Berry, Scott A. / Horvath, Thomas J. / Weilmuenster, K. James et al. | NTRS | 2001


    X-38 experimental aeroheating at Mach 10

    Berry, Scott / Horvath, Thomas / Weilmuenster, K. et al. | AIAA | 2001


    X-34 Experimental Aeroheating at Mach 6 and 10

    Berry, S. A. / Horvath, T. J. / DiFulvio, M. et al. | British Library Conference Proceedings | 1998