A Hypersonic Strike Fighter (HSF) would provide many benefits over current fighters, including increased effectiveness and survivability. However, there are many design challenges to developing such a vehicle. Therefore the conceptual design of an HSF requires the development of new tools and methods to analyze and select vehicle concepts. A parametric method was developed to determine aerodynamic characteristics of hypersonic vehicles in a rapid, automated way. This parametric method and other tools were then used to select a baseline design and optimize this baseline for the notional mission.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    World Aviation Congress & Exposition ; 2000



    Publication date :

    2000-10-10




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Implementation of Parametric Anaylsis to the Aerodynamic Design of a Hypersonic Strike Fighter

    Mavris, D. N. / Graham, M. / Sociewty of Automotive Engineers of New York et al. | British Library Conference Proceedings | 2000



    Hyperloop Rarefied Anaylsis

    Derek S. Liechty | NTRS


    Joint Strike Fighter

    Online Contents | 1998


    Joint Strike Fighter

    Online Contents | 1997