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Results:
1-7
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Results: 7
Authors:
Friedmann, PP
de Terlizzi, M
Myrtle, TF
Citation: Pp. Friedmann et al., New developments in vibration reduction with actively controlled trailing edge flaps, MATH COMP M, 33(10-11), 2001, pp. 1055-1083
Authors:
Friedmann, PP
Carman, GP
Millott, TA
Citation: Pp. Friedmann et al., Magnetostrictively actuated control flaps for vibration reduction in helicopter rotors - Design considerations for implementation, MATH COMP M, 33(10-11), 2001, pp. 1203-1217
Authors:
Friedmann, PP
Presente, E
Citation: Pp. Friedmann et E. Presente, Active control of flutter in compressible flow and its aeroelastic scaling, J GUID CON, 24(1), 2001, pp. 167-175
Authors:
Myrtle, TF
Friedmann, PP
Citation: Tf. Myrtle et Pp. Friedmann, Application of a new compressible time domain aerodynamic model to vibration reduction in helicopters using an actively controlled flap, J AMER HELI, 46(1), 2001, pp. 32-43
Authors:
Guillot, DM
Friedmann, PP
Citation: Dm. Guillot et Pp. Friedmann, Fundamental aeroservoelastic study combining unsteady computational fluid mechanics with adaptive control, J GUID CON, 23(6), 2000, pp. 1117-1126
Authors:
Cribbs, RC
Friedmann, PP
Chiu, T
Citation: Rc. Cribbs et al., Coupled helicopter rotor/flexible fuselage aeroelastic model for control of structural response, AIAA J, 38(10), 2000, pp. 1777-1788
Authors:
Friedmann, PP
Citation: Pp. Friedmann, Renaissance of aeroelasticity and its future, J AIRCRAFT, 36(1), 1999, pp. 105-121
Risultati:
1-7
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