Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Niloofar Moradian"'
Publikováno v:
2022 Houston, Texas July 17-20, 2022.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4a1581d44fc251ea42d2816b83992af7
https://doi.org/10.13031/aim.202200971
https://doi.org/10.13031/aim.202200971
Publikováno v:
Wind and Structures An International Journal. 14:35-53
Spherical object in wind is a common scenario in daily life and engineering practice. The main challenge in understanding the aerodynamics in turbulent wind lies in the multi-aspect of turbulence. This paper presents a wind tunnel study, which focuse
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5750aee24713c3533aa5fcf86c874443
https://doi.org/10.12989/was.2011.14.1.035
https://doi.org/10.12989/was.2011.14.1.035
Autor:
Niloofar Moradian, Mergen H. Ghayesh
Publikováno v:
Archive of Applied Mechanics. 81:781-799
The dynamical response of axially moving, partially supported, stretched viscoelastic belts is investigated analytically in this paper. The Kelvin–Voigt viscoelastic material model is considered and material, not partial, time derivative is employe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4e6def0c9b2fb6df4b4cd9e180fb91bb
https://doi.org/10.1007/s00419-010-0446-3
https://doi.org/10.1007/s00419-010-0446-3
Publikováno v:
Experimental Thermal and Fluid Science. 33:460-471
The effects of freestream turbulence intensity and integral length scale as freestream turbulent parameters on the drag coefficient of a sphere were experimentally investigated in a closed circuit wind tunnel. The Reynolds number, Re = Ud/ν, was var
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a8964bd6580d81e3f9e95628271a214c
https://doi.org/10.1016/j.expthermflusci.2008.11.001
https://doi.org/10.1016/j.expthermflusci.2008.11.001
Publikováno v:
29th International Symposium on Shock Waves 2 ISBN: 9783319168371
The air intake is an important component of hypersonic airbreathing engines. It is essentially a converging duct decelerating and compressing airflow and supplying the compressed air to the engine’s combustor. Molder and Szpiro [1] proposed to use
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eae9a963b8ae081586de15bca09391f4
https://doi.org/10.1007/978-3-319-16838-8_37
https://doi.org/10.1007/978-3-319-16838-8_37
Publikováno v:
19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
In this work quasi-steady starting of Busemann intakes with overboard mass spillage is considered analytically and simulated numerically using 2D and 3D unstructured adaptive Euler finite-volume flow solvers. Two designs of Busemann intakes are under
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b129bd3c1173022539747d548f177100
https://doi.org/10.2514/6.2014-3227
https://doi.org/10.2514/6.2014-3227