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S8 Engenharia Aeroespacial |
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Titulo:
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A HYBRID METHOD FOR AEROELASTIC ANALYSIS IN TRANSONIC FLOW
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Resumo :
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AEROELASTIC ANALYSES OF A FIGHTER AIRCRAFT AND OF THE STANDARD AEROELASTIC WING AGARD 445.6 IN TRANSONIC FLOW ARE PRESENTED. THE ANALYSES WERE PERFORMED USING A FINITE ELEMENT MODEL AND A MODAL MODEL RESPECTIVELY. THE DOUBLET-LATTICE BASED MODULE IN NASTRAN(TM) WAS USED WITH AERODYNAMIC INFLUENCE COEFFICIENTS MODIFIED FOR TRANSONIC FLOW ANALYSIS. THE AERODYNAMIC MODIFICATION WAS BASED ON RESULTS FROM A FINITE-DIFFERENCE NAVIER-STOKES SIMULATION OF FLOW AROUND THE WINGS IN TRANSONIC FLOW. |
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Autores :
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Mello, Olympio A. F.
Silva, Roberto G. A.
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Trabalho Completo :
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