Nonlinear, unsteady aerodynamic loads on rectangular and delta wings
Nonlinear, unsteady aerodynamic loads on rectangular and delta wings
- New search for: Atta, E. H.
- New search for: Kandil, O. A.
- New search for: Mook, D. T.
- New search for: Nayfeh, A. H.
- New search for: Atta, E. H.
- New search for: Kandil, O. A.
- New search for: Mook, D. T.
- New search for: Nayfeh, A. H.
Nonlinear unsteady aerodynamic loads on rectangular and delta wings in an incompressible flow are calculated by using an unsteady vortex-lattice model. Examples include flows past fixed wings in unsteady uniform streams and flows past wings undergoing unsteady motions. The unsteadiness may be due to gusty winds or pitching oscillations. The present technique establishes a reliable approach which can be utilized in the analysis of problems associated with the dynamics and aeroelasticity of wings within a wide range of angles of attack.
Document information
Nonlinear, unsteady aerodynamic loads on rectangular and delta wings
Aerospace Sciences Meeting ; 1977 ; Los Angeles, CA
1977-01-01
Conference paper
No indication
English
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