Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Ercan Dumlupinar"'
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2cdb340e1bf3884b90ca6b5e9eeb210d
https://doi.org/10.2514/6.2023-0028
https://doi.org/10.2514/6.2023-0028
Autor:
Jeffrey A. Housman, Stephen J. Alter, Ercan Dumlupinar, Bil Kleb, Greg J. Brauckmann, Mihirkumar M. Patel, James R. Koch, Cetin C. Kiris
Publikováno v:
AIAA AVIATION 2021 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::46f81dca3164f499225f4f1c342fb42c
https://doi.org/10.2514/6.2021-2966.c1
https://doi.org/10.2514/6.2021-2966.c1
Autor:
James R. Koch, Ercan Dumlupinar, Jeffrey A. Housman, Cetin C. Kiris, Mihirkumar M. Patel, Bil Kleb, Greg J. Brauckmann, Stephen J. Alter
Publikováno v:
AIAA AVIATION 2021 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0336ac77f5761120c38cc0496ffe8e65
https://doi.org/10.2514/6.2021-2966
https://doi.org/10.2514/6.2021-2966
Autor:
V. R. Murthy, Ercan Dumlupinar
Publikováno v:
46th AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c38ed6e0597afde3b888fd4f5c45a7dc
https://doi.org/10.2514/6.2008-386
https://doi.org/10.2514/6.2008-386
Autor:
Ercan Dumlupinar, V. R. Murthy
Publikováno v:
25th AIAA Applied Aerodynamics Conference.
In this work, the transonic unsteady aerodynamics calculations associated with simple harmonic pitching, indicial response to a step change in angle of attack, for NACA 64A010 airfoil are computed using CFD based on RANS. The parametric efiect of Spa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc273909206ecda2cef932c74015e96e
https://doi.org/10.2514/6.2007-4181
https://doi.org/10.2514/6.2007-4181
Autor:
V. R. Murthy, Ercan Dumlupinar
Publikováno v:
36th AIAA Fluid Dynamics Conference and Exhibit.
The NLR 7223-62 airfoil is a high speed airfoil with peaky leading edge contour. The high lift performance needed for helicopter applications is achieved by an inverse camber at the trailing edge. In this paper, unsteady ∞ow flelds of this airfoil
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6d147cb351545feeff5c1b2838d5eab5
https://doi.org/10.2514/6.2006-3375
https://doi.org/10.2514/6.2006-3375