The present work is concerned with predicting the unsteady flow considered to be the cause of the structural failure of twin vertical tail aircraft. An engineering tool has been produced for high angle of attack aerodynamics using the simplest physical models. The main innovation behind this work is its emphasis on the modeling of two key aspects of the dominant physics associated with high angle-of-attack airflows, namely unsteady separation and vortex breakdown.
Development of an engineering level prediction method for high angle of attack aerodynamics
AIAA, Aerospace Sciences Meeting and Exhibit ; 1993 ; Reno, NV, United States
1993-01-01
Conference paper
No indication
English
High Angle of Attack Aerodynamics
NTIS | 1994
|High Angle of Attack Aerodynamics
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|High Angle of Attack Aerodynamics
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