- 101 -
Bibliografia
[1] A. L. Erickson, J. D. Stephenson (1947): A suggested method of analyzing for transonic flutter of control surfaces based on available experimental evidence, N.A.C.A. Research Memo.
[2] H.W. Liepmann, A.Roshko (1957): Elements of gasdynamics, Wiley, New York, NY.
[3] G.Buresti: Fluidodinamica, Dispense dalle lezioni, Università degli Studi di Pisa, DIA.
[4] F. Sabetta: Gasdinamica, ed. Ingegneria 2000, Università di Roma “La Sapienza”.
[5] W.C. Griffith, W. Bleakney (1954): Shock Waves in Gases, Palmer Physical Laboratory, Princeton University, New Jersey.
[6] G. Jagadeesh: Fascinating word of shock waves, IISC, Banglore.
[7] E. Camilo, F.D. Marques, J.L.F. Azevedo (2008): Dynamic analysis of aeroelastic response for transonic flow with nonlinear structural model, ICAS 2008.
[8] C.A. Popescu, Y.S.Wong, B.H.K. Lee: System identification for nonlinear aeroelastic models.
[9] J.C. Kiiskila, M.R. Duncan, D.M. Pitt: Investigation of the dynamic characterization of aircraft control surface free play, The Boeing Company, St. Louis.
[10] J.Délery, J.G. Marvin, E.Reshotko (1986): Shock-wave boundary layer interactions, AGARDograph No. 280, Loughtnon, Essex.
[11] J. Délery, J. P. Dussauge (2009): Some physical aspects of shock wave/boundary layer interactions, Springer-Verlag.
[12] N.C. Lambourne (1964): Control-Surface Buzz, Aeronautical Research Council, Reports and Memoranda.
[13] N.C. Lambourne (1958): Some instabilities arising from the interactions between shock waves and boundary layers, AGARD Report 182.
[14] A. Frediani: Lezioni di Aeroelasticità, Università degli Studi di Pisa, Dispense.
[15] G. Bindolino, P. Mantegazza, P.Masarati: Aeroelasticità Applicata, Politecnico di Milano, Dispense.
[16] L.Morino, F. Mastroddi (2009): Course notes on structural dynamics for aerospace structures, Dispense.
- 102 -
[17] M. D. Conner, D. M. Tang, E. H. Dowell, L.N. Virgin (1996): Non linear behavior of a typical airfoil section with control surface freeplay: A numerical and experimental study, Duke University, Durham, USA.
[18] S. T. Trickey, L. N. Virgin, E. H. Dowell (2001): The stability of limit-cycle oscillations in a nonlinear aeroelastic system, Duke University, Durham, USA.
[19] R.E. Bartels: Development of Advanced Computational Aeroelasticity Tools at NASA Langley Research Center, NASA Langley Research Center, Hampton, USA.
[20] P. Mantegazza: Appunti del Corso di Aeroelasticità Applicata, Politecnico di Milano, Dispense.
[21] G. Buresti: Appunti dalle lezioni del corso di fluidodinamica, Università degli studi di Pisa.
[22] G. K. Batchelor: An introduction to fluid dynamics, Cambridge Mathematical Library.
[23] C. P. T. Groth (2010): Turbolence Modelling, AER1310.
[24] Ansys Fluent 12.0 Theory Guide.
[25] P. R. Spalart, S. R. Allmaras (1992): A one-equation turbulence model for aerodynamic flows, Technical Report AIAA-92-0439.
[26] T. Javaherchi (2010): A review of Spalart-Allmaras turbulence model and its modifications, Abstract, Department of Mechanical Engineering University of Washington.
[27] V. W. Nee, L. S. G. Kovasznay (1969): Simple phenomenological theory of turbulent shear flows, Physics of fluids, 12:473-484.
[28] J. Donéa (1983): Arbitrary Lagrangian-Eulerian finite element methods, Computational Methods Transient Analysis, Elsevier Science Publisher, Amsterdam.
[29] P. D. Thomas, C. K. Lombard (1979): Geometric conservation law and its application to flow computation on moving grids, AIAA Journal No 17.
[30] P. Di Marco: Termfluidodinamica applicata, Università degli Studi di Pisa.
[31] L. Cavagna (2007): NAEMO-CFD Theoretical Guide, Dipartimento di Ingegneria Aerospaziale, Politecnico di Milano.
[32] L. Cavagna (2007): NAEMO-CFD User’s Guide, Dipartimento di Ingegneria Aerospaziale, Politecnico di Milano.
[33] M. B. Giles (1997): Stability and accuracy of numerical boundary conditions in aeroelastic analysis, International Journal of Numerical Methods in Fluids.
[34] K. Sibilski, J. Zurek, W. Wroblewski: Influence of freeplay and friction in control system on aircraft flight dynamics, Articolo, ICAS 2008.
