The present study, which has demonstrated the feasibility of using time-resolved laser-induced fluorescence methods to ascertain boundary layer temperature distributions in real time for hypersonic vehicles in atmospheric flight, employs conventional optics in combination with novel time-resolved spectroscopy. The radiative lifetime and signal intensity involved, both of which are reduced by quenching, are adequate for measurement with state-of-the-art time-resolved fluorescence techniques, except for certain conditions associated with both the highest speeds and the lowest altitudes.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Fluorescence spectroscopy and thermometry for hypersonic flight research


    Contributors:

    Conference:

    AIAA/SFTE/DGLR/SETP Biannual Flight Test Conference ; 1990 ; Ontario, CA, United States


    Publication date :

    1990-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Fluorescence spectroscopy and thermometry for hypersonic flight research

    THOMPSON, B. / FERNANDEZ, S. / GUIGNON, E. | AIAA | 1990


    Nitric Oxide Planar Laser-Induced Fluorescence Thermometry in a Hypersonic Boundary Layer

    Connor C McDougall / W Schuyler Hinman / Craig T Johansen et al. | NTRS


    Nitric Oxide Planar Laser-Induced Fluorescence Thermometry Measurements in a Hypersonic Boundary Layer

    McDougall, Connor C. / Hinman, William S. / Johansen, Craig T. et al. | AIAA | 2018


    Pegasus Hypersonic Flight Research

    Budd, Gerald D. / Curry, Robert E. / Meyer, Robert R. | SAE Technical Papers | 1992


    Pegasus hypersonic flight research

    Curry, Robert E. / Meyer, Robert R., Jr. / Budd, Gerald D. | NTRS | 1992