Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Sutikno Wirogo"'
Autor:
Balasubramanyam Sasanapuri, Manish Kumar, Angela Lestari, Konstantin Kurbatskii, Sutikno Wirogo
Publikováno v:
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
The problem of a three-dimensional massively separated flow behind the Apollo capsule in a supersonic flow at different angles of attack is studied computationally using the general purpose CFD code ANSYS Fluent. Density-based and pressure-based coup
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::890f10da173eb66511040a27b749ed2f
https://doi.org/10.2514/6.2013-643
https://doi.org/10.2514/6.2013-643
Publikováno v:
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
The prototyping and testing of a supersonic cruise nozzle that covers wide range of nozzle geometry configurations (to help with large operating envelop of an aircraft) is both time consuming and expensive. Numerical simulations offer quick and less
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7173871d7b6be97b5818fa7454637610
https://doi.org/10.2514/6.2013-492
https://doi.org/10.2514/6.2013-492
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
turbulence model is employed to simulate turbulence effects. The near-wall mesh is fine enough to resolve the viscosity-affected near-wall region all the way to the laminar sublayer. A solution-based adaptive mesh refinement is applied to incr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6e2d3b316bde39fd9cb41f371bf68605
https://doi.org/10.2514/6.2012-863
https://doi.org/10.2514/6.2012-863
Publikováno v:
43rd AIAA Aerospace Sciences Meeting and Exhibit.
Based on previous experience of the use of different mesh topologies (hexahedral, tetrahedral and hybrid), the present work provides a study on refinement strategies for impingement limits computation. Although hexahedral meshes are more accurate in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5ca0dff9ac0217fc3f60bbf2a3940b67
https://doi.org/10.2514/6.2005-1247
https://doi.org/10.2514/6.2005-1247
Autor:
Luis Santos, Antonio Batista de Jesus, Sutikno Wirogo, Ramon Papa, Guilherme Lara Oliveira, Luiz Tobaldini
Publikováno v:
42nd AIAA Aerospace Sciences Meeting and Exhibit.
The present work compares the effects on accuracy of different grid generation choices and practices with respect to collection efficiency calculation on a typical aircraft configuration. It is known that hexahedral mesh es provide more accurate and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d155f2530ce3f74e350321669fe415af
https://doi.org/10.2514/6.2004-566
https://doi.org/10.2514/6.2004-566
Publikováno v:
41st Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::40570b351f0420d74e4d4b40acb471b3
https://doi.org/10.2514/6.2003-1073
https://doi.org/10.2514/6.2003-1073
Autor:
Sutikno Wirogo, Ganesh Rajagopalan
Publikováno v:
13th Computational Fluid Dynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7cd328b7345f0daa95a889a93b482553
https://doi.org/10.2514/6.1997-2033
https://doi.org/10.2514/6.1997-2033