Aerodynamic Loads of Small-Amplitude Pitching NACA 0012 Airfoil at Reynolds Number of 1000

Date

2018-08-01

Author

Kurtuluş, Dilek Funda

Metadata

Show full item record

This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Item Usage Stats

119
views

0
downloads

URI

https://hdl.handle.net/11511/48738

Journal

AIAA JOURNAL

DOI

https://doi.org/10.2514/1.j056879

Collections

Department of Aerospace Engineering, Article

Suggestions

OpenMETU
Core

Aerodynamic measurements of a morphing wing Özçakmak, Özge Sinem; Özgen, Serkan (null; 2015-09-10)
Aerodynamic parameter estimation of a missile Aksu, Arda; Kutay, Ali Türker; Department of Aerospace Engineering (2013) Aerodynamic characteristics of missiles depend strongly on wind angles, that is, angle of attack and sideslip angle. However it is impractical to measure these angles during missile testing. Therefore, without direct information of the wind angles, it becomes a difficult problem to be able to accurately estimate the missile aerodynamic parameters from flight tests. This thesis addresses this problem and suggests an approach to estimate missile aerodynamic parameters successfully without wind angles measurem...
Aerodynamic Analyses of Thick Wind Turbine Airfoils for High Reynolds Numbers ASLAN, EZGİ; Orbay Akcengiz, Ezgi; Sezer Uzol, Nilay (2021-09-08) In this study, Computational Fluid Dynamics simulations of flow around thick have been performed. Thick airfoils are generally preferred in wind turbine blades for structural and aerodynamic performances. High Reynolds flows around thick airfoils are one of the challenging problems in wind turbine blade design due to turbulent, separated and complex flow field characteristics. In the CFD analyses, both 2-D RANS simulation approach on structured computational grids is considered. Grid sensitivity study is al...
Aerodynamic characteristics of an airfoil oscillating in pitch. Solakoğlu, Erhan; Department of Aeronautical Engineering (1987)
Aerodynamic parameter estimation of a supersonic air to air missile with rapid speed variation Bayoglu, Tugba; Nalci, Mehmet Ozan; Kutay, Ali Türker (2016-01-01) © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.Maneuver inputs designed for aircraft parameter identification are often applied during the aircraft flies close to a trimmed flight condition at an approximately constant Mach number. Since a fixed wing aircraft has control over its thrust and speed, various maneuver inputs can be applied to identify aerodynamic derivatives at discrete Mach numbers. On the contrary, most agile missile configurations do not have contr...

Citation Formats

D. F. Kurtuluş, “Aerodynamic Loads of Small-Amplitude Pitching NACA 0012 Airfoil at Reynolds Number of 1000,” AIAA JOURNAL, pp. 3328–3331, 2018, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/48738.