Biblio

Found 7 results
[ Author(Asc)] Keyword Type Year
Filters: First Letter Of Keyword is A and Author is Lorenzo Pinelli  [Clear All Filters]
A B C D E F G H I J K L M N O P Q R S T U V W X Y Z 
P
Pinelli L, Marconcini M, Arnone A, Bacci D.  Submitted.  High Fidelity Modeling of Acoustic Liners For Aeronautical Applications. 34th Congress of the International Council of the Aeronautical Sciences.
Pinelli L, Burberi C, Ignesti M, Michelassi V, Tapinassi L, Abati A, Pacciani R.  2023.  Forced response in a multi-stage aeroderivative axial compressor with acoustic excitations: Method validation with field data. Aerospace Science and Technology. 138
Pinelli L, Amedei A, Meli E, Vanti F, Romani B, Benvenuti G, Fabbrini M, Morganti N, Rindi A, Arnone A.  2022.  Innovative Design, Structural Optimization and Additive Manufacturing of New-Generation Turbine Blades. ASME J. Turbomach.. 144(1):011006.
Pinelli L, Vanti F, Arnone A, Bessling B, Vogt D.  2019.  Influence of tip shroud modeling on the flutter stability of a low pressure turbine rotor. ASME Turbo Expo 2019. Volume 7A: Structures and Dynamics:V07AT36A012.
ASME paper GT2019-91204
Pinelli L, Burberi C, Ignesti M, Michelassi V, Tapinassi L, Abati A, Pacciani R.  2023.  Forced response in a multi-stage aeroderivative axial compressor with acoustic excitations: Method validation with field data. Aerospace Science and Technology. 138
Pinelli L, Marconcini M, Pacciani R, Bake F, Knobloch K, Gaetani P, Persico G.  2022.  Effect of Clocking on Entropy Noise Generation Within an Aeronautical High Pressure Turbine Stage. J.Sound Vib.. 529(116900)
Pinelli L, Marconcini M, Arnone A, Bacci D.  Submitted.  High Fidelity Modeling of Acoustic Liners For Aeronautical Applications. 34th Congress of the International Council of the Aeronautical Sciences.