Experimental Investigation of Local Flexible Surface on Aerodynamic Effects for Finite Wing with NACA0018 Section

Çukurova Üniversitesi Mühendislik Fakültesi Dergisi, Journal Year: 2025, Volume and Issue: 40(1), P. 61 - 68

Published: March 26, 2025

The experimental study is conducted in low-speed wind tunnel order to explore the effects of flexible surface on aerodynamic performance NACA0018 finite wing. In this purpose, lift and drag force wing measured using six axes load cell over angle attack 0°-18° at different Reynolds numbers. Moreover, oil flow visualization experiments are performed depict structure remarkably improves Re=3×104, it also enhances coefficient diminishes coefficient. stall delayed from 2.5° 7°. It observed that shifted further when number increased. However, effect with increasing number. Furthermore, tip vortex laminar separation bubble significantly influence structure.

Language: Английский

Investigation of behavior of the jet engine blades under heat and pressure effects with fluid structure interaction analyses

Thermal Science and Engineering Progress, Journal Year: 2025, Volume and Issue: unknown, P. 103601 - 103601

Published: April 1, 2025

Language: Английский