Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Roberto F. Bobenrieth Miserda"'
Autor:
Ana Luisa P. Maldonado, Jon Sims, Ben Cox, Braulio G. Pimenta, Roberto F. Bobenrieth Miserda, Joy Stevens, Tanisha Mascarenhas
Publikováno v:
28th AIAA/CEAS Aeroacoustics 2022 Conference.
Publikováno v:
28th AIAA/CEAS Aeroacoustics 2022 Conference.
Publikováno v:
Journal of Propulsion and Power. 36:363-380
The first objective of this work is the verification of a moving-body immersed boundary method for the direct computation of noise generated by rotor-stator interactions in transonic 2-D cascades. ...
Publikováno v:
Journal of Propulsion and Power. 35:530-543
The objective of this work is the validation of a moving-body immersed boundary methodology used for the calculation of multiple pure tone noise generated by supersonic rotor cascades. This methodo...
Publikováno v:
25th AIAA/CEAS Aeroacoustics Conference.
Publikováno v:
21st AIAA/CEAS Aeroacoustics Conference.
The objective of this work is the validation of an immersed boundary methodology used for the calculation of the multiple pure tone noise generated by supersonic rotor cascades. This methodology is based on a discrete forcing approach where the bound
Publikováno v:
20th AIAA/CEAS Aeroacoustics Conference.
A surface interpolation scheme that has a formal fourth-order precision in space and has no amplification in the frequency domain is used to directly compute the linear and nonlinear rotor-stator interaction modes in transonic cascades. The time-depe
Autor:
Rafael L. Bites, Braulio Gutierrez Pimenta, Roberto F. Bobenrieth Miserda, Ana Luisa P. Maldonado
Publikováno v:
19th AIAA/CEAS Aeroacoustics Conference.
The objective of this work is the validation of a moving-body fourth-order immersed boundary method for direct tonal noise predictions of rotor-stator interactions in twodimensional cascades. The time-dependent and compressible Euler equations are nu
Publikováno v:
The Journal of the Acoustical Society of America. 140:3321-3321
In this work, time domain boundary conditions of wall impedance are simulated on circular and annular ducts of constant cross section. The discretization technique used here is the immersed boundary method in the framework of finite volume formulatio
Publikováno v:
18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference).