Radespiel, R. (1994) Aerodynamic Design of Supersonic Wings with High Aerodynamic Efficiency. 7th European Aerospace Conference EAC'94.
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The design of supersonic waveriders with high aerodynamic efficiency is investigated. This approach is motivated by the high wing aspects ratios obtained with supersonic leading edges as compared to the traditional subsonic leading edges. Moreover, the choice of supersonic leading edges may pave the way to laminar flow with low friction drag, because it is believed that the boundary layers exhibit low levels of crossflow. Sensitivity analysis of the aerodynamic efficiency of supersonic waveriders with respect to design lift, wing aspect ratio and planform shape is presented. Stability analysis of the laminar boundary layers near the leading edge is used to assess the relative importance of streamwise and crossflow instabilities. The results obtained so far indicate that waverider designs are promising for supersonic transport configurations.
|Document Type:||Conference or Workshop Item (Paper)|
|Additional Information:||LIDO-Berichtsjahr=1994, pages=10,|
|Title:||Aerodynamic Design of Supersonic Wings with High Aerodynamic Efficiency|
|Keywords:||Supersonic flow, wing design, waverider, aerodynamic efficiency, laminar flow, boundary-layer stability|
|Event Title:||7th European Aerospace Conference EAC'94|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||Space (old)|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||UNSPECIFIED|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||W - Grundlagen Raumtransport - Anlagen und Messtechnik (old)|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||03 Apr 2006|
|Last Modified:||27 Apr 2009 10:05|
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