Virtual aeroelastic flight testing for the F-16 fighter with stores
Publication
, Conference
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
ISBN
9781563478918
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 - US 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 - US 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
ISBN
9781563478918
Publication Date
November 5, 2007
Start / End Page
339 / 346