The growing attention of supersonic transport (SST) renews economic and environmental concerns. New designs shall improve flight efficiency as well as mission, air traffic management (ATM) air traffic service (ATS) impact, requiring a flexible and collaborative approach. A conceptual design tool linking to varied fidelity domain is developed in DLR since 2005. The focus areas of this paper are: -) Expanding openAD to design and evaluate future SST Aircraft within a higher-fidelity workflow -) Capabilities demonstration of openAD via sensitivity studies of reference vehicle Concorde, HIASC A, HICAC C and X-59A (publicly available data)


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    Titel :

    Development of a Conceptual Design Tool for Supersonic Transport with a Variable Fidelity Interface


    Beteiligte:
    Dietl, T. (Autor:in) / Schnell, S. (Autor:in) / Shiva Prakasha, P. (Autor:in) / Nagel, B. (Autor:in) / Brodersen, O. (Autor:in)

    Erscheinungsdatum :

    2023


    Format / Umfang :

    11 pages



    Medientyp :

    Sonstige


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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