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- W2045646835 abstract "An experimental identi cation investigation of unsteady and stall aerodynamic coef cients for an external store of an aircraft has been made. The coef cient identi cation is performed by a least-squares procedure based on the measured time series obtained from an aeroelastic model undergoing aerodynamic excitation caused by a gust generator. The results are veri ed by the good correlation between the theoretical prediction and aerodynamic measurement data. Using the identi ed unsteady aerodynamic model, numerical investigations for both the stability ( utter) and nonlinear aeroelastic response of this external store model have been made. Also, the results were compared with those obtained from a quasisteady aerodynamic model. It is seen that the effects of unsteady aerodynamics on the nonlinear aeroelastic response are signi cant when the angle of attack is large." @default.
- W2045646835 created "2016-06-24" @default.
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- W2045646835 date "1998-09-01" @default.
- W2045646835 modified "2023-09-23" @default.
- W2045646835 title "Unsteady Aerodynamic Forces and Aeroelastic Response for External Store of an Aircraft" @default.
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- W2045646835 doi "https://doi.org/10.2514/2.2377" @default.
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