Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Avinash Jammalamadaka"'
Autor:
Benjamin M. Duda, Long He, Jose Escobar, Avinash Jammalamadaka, Wende Li, John Wanderer, Yanbing Li, Gregory M. Laskowski
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29116ef9192cf75aa1ca7479b84c7bce
https://doi.org/10.2514/6.2022-2197
https://doi.org/10.2514/6.2022-2197
Autor:
Gregory M. Laskowski, Avinash Jammalamadaka, Chen Hudong, Yanbing Li, Pradeep Gopalakrishnan, Raoyang Zhang, James E. Kopriva
Publikováno v:
AIAA AVIATION 2020 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bd77e66a38a2473453b03b762008c75c
https://doi.org/10.2514/6.2020-3055
https://doi.org/10.2514/6.2020-3055
Autor:
Emmanuel Vanoli, Avinash Jammalamadaka, Yoann Mery, Michel Nocture, Pradeep Gopalakrishnan, Javier Ruiz Domingo, Nicolas Rochuon, Benoît Bonnal
Publikováno v:
Volume 2A: Turbomachinery.
Modeling of the engine behavior in windmilling conditions is an important engineering objective. The relight capability of the engine is mainly associated with the air mass flow rate that passes through the engine high pressure core in those conditio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b988929af16f1ac6dcdd060150567d9a
https://doi.org/10.1115/gt2019-90465
https://doi.org/10.1115/gt2019-90465
Autor:
Wouter C. van der Velden, Damiano Casalino, Avinash Jammalamadaka, Raoyang Zhang, Pradeep Gopalakrishnan, Yanbing Li, Hudong Chen
Publikováno v:
2018 AIAA/CEAS Aeroacoustics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::edaf534ae120b8c432da98798eaedf65
https://doi.org/10.2514/6.2018-3617
https://doi.org/10.2514/6.2018-3617
Publikováno v:
2018 Fluid Dynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a302a0aa65ab8095838fa136dcb3b2d2
https://doi.org/10.2514/6.2018-4030
https://doi.org/10.2514/6.2018-4030
Autor:
Avinash Jammalamadaka, Farhad Jaberi
Publikováno v:
Theoretical and Computational Fluid Dynamics. 29:29-54
Data generated by direct numerical simulation (DNS) for a Mach 2.75 zero-pressure gradient turbulent boundary layer interacting with shocks of different intensities are used for a priori analysis of subgrid-scale (SGS) turbulence and various terms in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ee4bfb02fdff9f3beb571e065e5a1ae8
https://doi.org/10.1007/s00162-015-0339-8
https://doi.org/10.1007/s00162-015-0339-8
Autor:
Raoyang Zhang, Pardeep Gopalakrishnan, Hudong Chen, Benedikt Konig, Avinash Jammalamadaka, Deepali Singh, Yanbing Li, Ehab Fares, Angela Ribeiro
Publikováno v:
Delft University of Technology
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8b050b7405ea6477f57b6324446cb32c
https://doi.org/10.2514/6.2017-1438
https://doi.org/10.2514/6.2017-1438
Publikováno v:
AIAA Journal. 51:1174-1188
Direct numerical simulation and large-eddy simulation of a flat-plate supersonic turbulent boundary layer interacting with an oblique incident shock wave are conducted for a priori and a posteriori assessments of subgrid-scale models. The incident sh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::36b7964f3d652c20df24d90e41aed575
https://doi.org/10.2514/1.j051955
https://doi.org/10.2514/1.j051955
Autor:
Yanbing Li, Avinash Jammalamadaka
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
A Lattice-Boltzmann Methods (LBM) coupled with a very large eddy simulation (VLES) is presented and applied to solve complex aero-thermal problems in generic turbo-machinery devices. Simple 1D Sod problem, 2D converge-diverge nozzle problem and 2D tr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c164b86c49bb89edd2be8402e5a1e051
https://doi.org/10.2514/6.2015-4128
https://doi.org/10.2514/6.2015-4128
Publikováno v:
44th AIAA Fluid Dynamics Conference.
This paper presents an investigation of the NACA 4412 trailing edge separation test case using the Lattice-Boltzmann code PowerFLOW. It is shown that the method, which does not predict the separation in two-dimensional simulations, delivers good resu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d43348ea7909ae9190657879a20a9cf7
https://doi.org/10.2514/6.2014-3324
https://doi.org/10.2514/6.2014-3324