Transonic aerodynamic loads modeling of X-31 aircraft pitching motions
The generation of reduced-order models for computing the unsteady and nonlinear aerodynamic loads on an aircraft from pitching motions in the transonic speed range is described. The models considered are based on Duhamel's superposition integral using indicial (step) response functions, Volterr...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
2013.
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| Subjects: | |
| Online Access: | Get fulltext |