Aerothermal modeling is inherently entwined with TPS design. Aerothermal, radiation, and TPS material response are coupled so it's important to check modeling assumptions. Validation of numerical models using ground and flight tests is important to quantify uncertainties. A margin policy based on statistical methods may provide greater insight in the key drivers and overall reliability of the design


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aerothermal Considerations for Entry, Descent, and Landing


    Contributors:
    Tang, Chun (author)

    Conference:

    Thermal and Fluids Analysis Workshop (TFAWS) ; 2015 ; Silver Spring, MD, United States


    Publication date :

    2015-08-03


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Aerothermal Modeling Challenges for Entry Descent and Landing Missions

    Wright, Michael J. / Hollis, Brian R. / Barnhardt, Michael D. et al. | NTRS | 2018


    AERODYNAMIC AND AEROTHERMAL ENVIRONMENT MODELS FOR A MARS ENTRY, DESCENT, AND LANDING SYSTEMS ANALYSIS STUDY

    Kinney, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011



    Entry, Descent, and Landing

    Chen, Allen | NTRS | 2013