Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    AIAA-2007-1186 PRANDTL/SCHMIDT NUMBER EFFECT ON TEMPERATURE DISTRIBUTION IN A MODEL COMBUSTOR



    Conference:

    18th, International symposium on air breathing engines IASBE ; 2007 ; Beijing, China



    Publication date :

    2007-01-01


    Size :

    89 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Detailed Measurement of ORSC Main Chamber Injector Dynamics in a Model Rocket Combustor (AIAA 2018-1186)

    Bedard, Michael J. / Austin, Benjamin J. / Anderson, William E. | British Library Conference Proceedings | 2018


    Nr. 1186

    DataCite | 1868

    Free access


    LES of a Supersonic Combustor with Variable Turbulent Prandtl and Schmidt Numbers

    Ingenito, A. / Bruno, C. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008


    AIAA-2001-1186 Composite Sandwich Beams Under Low-Velocity Impact

    Abot, J. / Daniel, I. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2001