Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    AIAA-2004-4837 Validation of Inlet and Exhaust Boundary Conditions for a Cartesian Method


    Contributors:
    Pandya, S. (author) / Murman, S. (author) / Aftosmis, M. (author)

    Conference:

    22nd, AIAA applied aerodynamics conference ; 2004 ; Providence, RI



    Publication date :

    2004-01-01


    Size :

    16 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Validation of Inlet and Exhaust Boundary Conditions for a Cartesian Method

    Pandya, Shishir / Murman, Scott / Aftosmis, Michael | AIAA | 2004


    Nr. 4837

    DataCite | 1938


    Numerical Simulation of an Aircraft Engine Intake S-Duct Diffuser (AIAA 2017-4837)

    Selvanayagam, Jeyatharsan / Aliaga, Cristhian / Stokes, John et al. | British Library Conference Proceedings | 2017


    AIAA-2002-4837 Reconfigurable Helicopter Flight Control Methods for Main Rotor Actuator Failures

    Si, J. / Enns, R. / AIAA | British Library Conference Proceedings | 2002


    AIAA-2004-5380 Hypersonic Inlet Flow Analysis at Off-Design Conditions

    Bachchan, N. / Hillier, R. | British Library Conference Proceedings | 2004