Critical Angle and Fundamental Frequency of Symmetric Airfoils at Low Reynolds Numbers

Autor: D. F. Kurtulus

Publikováno v: Journal of Applied Fluid Mechanics, Vol 15, Iss 3, Pp 723-735 (2022)

The unsteady vortex evolution of NACA 0012 airfoil is numerically investigated at low angles of attack ranging from 0° to 10° where the separation is performed from the trailing edge. The Reynolds number ranges between 1000 and 4000. The laminar se

Externí odkaz: https://doaj.org/article/2f74ce768f934e2b8087840f1774514d

Improving the quality of biogas fuel combustion in a household gas burner.

Autor: Ramazanov, R.S., Suslov, D.Y., Kushchev, L.A.

Publikováno v: BIO Web of Conferences; 4/17/2024, Vol. 103, p1-5, 5p

Membrane Separations in Biomass Processing.

Autor: Mandalika AS; Assistant Research Professor, Center for Energy Studies, Louisiana State University, 93 S Quad Dr, 1115, Baton Rouge, LA 70803., Runge TM; Professor of Biological Systems Engineering and CALS Associate Dean for Research, 2121 Wisconsin Energy Institute Building, University of Wisconsin-Madison, 1552 University Ave, Madison, WI 53726., Ragauskas AJ; Governor's Chair for Biorefining, Joint Institute for Biological Sciences, Biosciences Division, Oak Ridge National Laboratory, 1 Bethel Valley Road, Oak Ridge, TN 37831.

Publikováno v: ChemPlusChem [Chempluschem] 2024 Oct 28, pp. e202400497. Date of Electronic Publication: 2024 Oct 28.

The effect of adding floaters to airplane models on aerodynamic characteristics using computational fluid dynamics methods.

Autor: Kusuma, Yudiawan Fajar, Defianti, Hanni, Syamsuar, Sayuti

Publikováno v: AIP Conference Proceedings; 2023, Vol. 2941 Issue 1, p1-10, 10p

Numerical study of new techniques drag reduction: application to aerodynamic devices.

Autor: Agriss, Amine¹ amineagriss@research.emi.ac.ma, Agouzoul, Mohamed¹, Ettaouil, Abdeslem¹, Mehdari, Abdessamad¹

Publikováno v: International Journal for Simulation & Multidisciplinary Design Optimization. 2021, Vol. 12, p1-11. 11p.