Zobrazeno 1 - 10
of 42
pro vyhledávání: '"NASA TRAP wing"'
Autor:
Wang, Zhongyuan
This project aims to study and perform a turbulent flow simulation over the NASA Trap Wing by exploring the numerical aerodynamic predictions capacity of high lift configurations using two S-A, k-ω SST and DES method for comparison in ANSYS Fluent s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od________70::722f4e6996580b2b4d7b98ada36d97ec
https://dspace.lib.cranfield.ac.uk/handle/1826/19447
https://dspace.lib.cranfield.ac.uk/handle/1826/19447
Publikováno v:
30th AIAA Applied Aerodynamics Conference.
The OVERFLOW computational fluid dynamics code is used to simulate a high lift flow field about the NASA Trap Wing wind tunnel model with the goal of better understanding bracket and boundary layer transition effects on prediction of aerodynamic load
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::63abe498943d81b0120878c20fdc1291
https://doi.org/10.2514/6.2012-2919
https://doi.org/10.2514/6.2012-2919
Publikováno v:
30th AIAA Applied Aerodynamics Conference.
The present paper consolidates the results of computations performed for NASA Trap Wing during two workshops, SPICES09 and HiLiftPW1 and addresses issues pertaining to CFD prediction of pitching moment and flow unsteadiness near stall angle. The conf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2ccf761cdc24552c566afd67c25695cc
https://doi.org/10.2514/6.2012-2849
https://doi.org/10.2514/6.2012-2849
Publikováno v:
29th AIAA Applied Aerodynamics Conference.
A computational analysis on the influence of the transition for the NASA Trap Wing Model has been carried out, which is an extension of the work presented for the 1 st AIAA High Lift Prediction Workshop. The transition prediction is based on stabilit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e6af1a743827231657f708f984d9f2e1
https://doi.org/10.2514/6.2011-3009
https://doi.org/10.2514/6.2011-3009
Publikováno v:
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
st AIAA CFD High Lift Prediction Workshop, the NASA Trap Wing wind tunnel model is analyzed using the Reynolds-averaged Navier-Stokes (RANS) flow solver OVERFLOW. A family of structured, overset grids built for the workshop consists of a coarse (10.7
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e12c0c1e534a80e3cf794b4e427bf4e3
https://doi.org/10.2514/6.2011-866
https://doi.org/10.2514/6.2011-866
Autor:
Carlos Silva, Juan Mahecha, Rodrigo A. Jiménez, Santiago Ramirez, Andres Mauricio Giraldo, Omar D. Lopez, Nicolas Ochoa-Lleras, Sebastián Leguizamón, Jaime A. Escobar
Publikováno v:
30th AIAA Applied Aerodynamics Conference.
This paper presents a contribution to the development of a methodology to accurately predict high lift wing con gurations using CFD. Initially, cases from the 1 AIAA High Lift Prediction Workshop were reproduced in order to validate the simulation pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::89e866c4c062191f50a9439fcb14d761
https://doi.org/10.2514/6.2012-2921
https://doi.org/10.2514/6.2012-2921
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