Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Visualization of Hypersonic Compression Corner Flows Using Temperature- and Pressure-Sensitive Paints AIAA Paper



    Kongress:

    45th, AIAA aerospace sciences meeting ; 2007 ; Reno, NV



    Erscheinungsdatum :

    01.01.2007


    Format / Umfang :

    2007-118-2007-599


    Anmerkungen:

    Papers in the range 2007 17 to 1467 with gaps. Held on CD-ROM


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    TEMPERATURE-CANCELLED ANODIZED-ALUMINUM PRESSURE SENSITIVE PAINT FOR HYPERSONIC COMPRESSION CORNER FLOWS

    Kuriki, T. / Sakaue, H. / Imamura, O. et al. | British Library Conference Proceedings | 2010


    Temperature-Cancelled Anodized-Aluminum Pressure Sensitive Paint for Hypersonic Compression Corner Flows

    Kuriki, Takuma / Sakaue, Hirotaka / Imamura, Osamu et al. | AIAA | 2010


    Development of Ultra-fast Temperature Sensitive Paints for Hypersonic High Speed Flows (AIAA 2017-2211)

    Schramm, Jan Martinez / Edzards, Frank / Hannemann, Klaus | British Library Conference Proceedings | 2017


    Computation of laminar hypersonic compression-corner flows

    Rudy, David H. / Thomas, James L. / Kumar, Ajay et al. | NTRS | 1991