Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Bedri Yagiz"'
Publikováno v:
34th AIAA Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6dcfe836c11c67ae747b66e5075c365d
https://doi.org/10.2514/6.2016-4336
https://doi.org/10.2514/6.2016-4336
Publikováno v:
34th AIAA Applied Aerodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c079b05ff10eb55bdbd0df3114a9d806
https://doi.org/10.2514/6.2016-4335
https://doi.org/10.2514/6.2016-4335
Autor:
Y. Volkan Pehlivanoglu, Bedri Yagiz
Publikováno v:
Aerospace Science and Technology. 23:479-491
A new optimization algorithm is proposed and tested for four different test cases: benchmark test functions, multi-element airfoil optimization in subsonic flow, active flow control parameter optimization in transonic flow, and a direct shape optimiz
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a6e12950c81916a0af45c1011c2486eb
https://doi.org/10.1016/j.ast.2011.10.006
https://doi.org/10.1016/j.ast.2011.10.006
Publikováno v:
International Journal of Thermal Sciences. 58:61-69
Heat convection from the uniformly heated walls of a straight channel in presence of a rotationally oscillating cylinder (ROC) is simulated at Re = 100. Heat transfer enhancement due to vortex shedding from the ROC is investigated. Systematic studies
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5ea1e8d07c6db02c6113d92130d6865e
https://doi.org/10.1016/j.ijthermalsci.2012.03.012
https://doi.org/10.1016/j.ijthermalsci.2012.03.012
Publikováno v:
Aerospace Science and Technology. 17:21-31
The objective of this paper is to appraise the practicability of weakening the shock wave and hereby reducing the wave drag in transonic flight regime using flow control devices such as two-dimensional contour bump, individual jet actuator, and also
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c08ce8f4d2612bd22f8d329cb2f8ed0d
https://doi.org/10.1016/j.ast.2011.03.003
https://doi.org/10.1016/j.ast.2011.03.003
Autor:
Bedri Yagiz, Y. Volkan Pehlivanoglu
Publikováno v:
Journal of Aircraft. 48:212-219
To improve aerodynamic performance, the active and passive flow control parameters are optimized in different combinations. The flow is simulated by solving the Navier–Stokes equations and a turbulence model. The active flow control is applied usin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::087939d914f72c3571034483ce7cf689
https://doi.org/10.2514/1.c031066
https://doi.org/10.2514/1.c031066
Publikováno v:
Journal of Aircraft. 47:1955-1965
To improve the aerodynamic performance, the control applied to the transonic flow past an airfoil is optimized. The flow is simulated by solving the Navier–Stokes equations and a turbulence model. The control is applied using flow suction or blowin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8aeabe2d0b9e70b761455d4578e980d3
https://doi.org/10.2514/1.c000233
https://doi.org/10.2514/1.c000233
Publikováno v:
22nd AIAA Computational Fluid Dynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b041326413eba7ef964773c18fe42615
https://doi.org/10.2514/6.2015-3422
https://doi.org/10.2514/6.2015-3422
Autor:
Bedri Yagiz, Osama A. Kandil
Publikováno v:
27th AIAA Applied Aerodynamics Conference.
Control of shock waves at transonic speed of a NACA 0012 is investigated via numerical solutions of the time-dependent turbulent–Spalart–Allmaras Navier-Stokes equations. The effects of surface suction/blowing on airfoil aerodynamic performance h
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1c867fb8a5749a885182de7fb978c5f2
https://doi.org/10.2514/6.2009-3763
https://doi.org/10.2514/6.2009-3763
Publikováno v:
45th AIAA Aerospace Sciences Meeting and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0a7760e2d2322e798fbab14bd8af307e
https://doi.org/10.2514/6.2007-1243
https://doi.org/10.2514/6.2007-1243