Results of Theodorsen and Garrick Revisited

Evidence is presented that some of the flutter boundaries (for the 2- and 3-DOF, 2D airfoil in incompressible, inviscid flow) found in the NACA reports by Theodorsen and Garrick are in error, and that many other might also be in error. It is suggested that the state of computational capabilities tha...

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Veröffentlicht in:Journal of aircraft 2000-09, Vol.37 (5), p.918-920
1. Verfasser: Zeiler, Thomas A
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description Evidence is presented that some of the flutter boundaries (for the 2- and 3-DOF, 2D airfoil in incompressible, inviscid flow) found in the NACA reports by Theodorsen and Garrick are in error, and that many other might also be in error. It is suggested that the state of computational capabilities that existed at the time the original NACA reports were prepared contributed in large measure to the errors. It is recommended that all of the plots in these classic and historically important NACA documents be recomputed and published. (CSA)
doi_str_mv 10.2514/2.2691
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subjects Exact sciences and technology
Fundamental areas of phenomenology (including applications)
Physics
Solid mechanics
Structural and continuum mechanics
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
Vibrations and mechanical waves
title Results of Theodorsen and Garrick Revisited
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