Virtual aeroelastic flight testing for the F-16 fighter with stores
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Thomas, JP; Dowels, EH; Hall, KC; Denegri, CM
Published in: Collection of Technical Papers U S Air Force T and E Days 2007 Test and Evaluation
November 5, 2007
In the following, we present computational aeroelastic flutter onset and limit cycle oscillation response trends for various stores and weapons configurations of the F-16 fighter. A nonlinear harmonic balance compressible Reynolds averaged Navier-Stokes computational fluid dynamic flow solver is used to model the unsteady aerodynamics of the F-16 wing. However, slender body/wing theory is used as an approximate method in accounting for the unsteady aerodynamic effects of wingtip launchers and missiles.
Duke Scholars
Published In
Collection of Technical Papers U S Air Force T and E Days 2007 Test and Evaluation
Publication Date
November 5, 2007
Start / End Page
339 / 346
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Thomas, J. P., Dowels, E. H., Hall, K. C., & Denegri, C. M. (2007). Virtual aeroelastic flight testing for the F-16 fighter with stores. In Collection of Technical Papers U S Air Force T and E Days 2007 Test and Evaluation (pp. 339–346).
Thomas, J. P., E. H. Dowels, K. C. Hall, and C. M. Denegri. “Virtual aeroelastic flight testing for the F-16 fighter with stores.” In Collection of Technical Papers U S Air Force T and E Days 2007 Test and Evaluation, 339–46, 2007.
Thomas JP, Dowels EH, Hall KC, Denegri CM. Virtual aeroelastic flight testing for the F-16 fighter with stores. In: Collection of Technical Papers U S Air Force T and E Days 2007 Test and Evaluation. 2007. p. 339–46.
Thomas, J. P., et al. “Virtual aeroelastic flight testing for the F-16 fighter with stores.” Collection of Technical Papers U S Air Force T and E Days 2007 Test and Evaluation, 2007, pp. 339–46.
Thomas JP, Dowels EH, Hall KC, Denegri CM. Virtual aeroelastic flight testing for the F-16 fighter with stores. Collection of Technical Papers U S Air Force T and E Days 2007 Test and Evaluation. 2007. p. 339–346.
Published In
Collection of Technical Papers U S Air Force T and E Days 2007 Test and Evaluation
Publication Date
November 5, 2007
Start / End Page
339 / 346