Evaluation and Selection of Aerofoil based on Flow Induced Vibration and Damping Ratio
Uthish Shankar S
, Maheswaran M , Nithin Kumar P , Vijey V S
Aerofoils, Performance characteristics, Supercritical Aerofoil, NACA0012, NACA SCA0714, ANSYS CFX, Flow induced vibration(FIV), Vibrational analysis, Fluid structure interface(FSI), Damping characteristics.
This paper deals with the evaluation and selection of aerofoils based on its performance characteristics. Two different type of aerofoils are used for testing such as ordinary aerofoil and supercritical aerofoil namely NACA0012 and NACA SCA0714 respectively are being considered for analysis. The tests are being conducted using ANSYS CFX Simulation software. The two aerofoils subjected to Flow induced vibration(FIV) for vibrational analysis using fluid structure interface(FSI). They are finally tested on their damping characteristics. These test results of both aerofoils are compared and results are concluded.
"Evaluation and Selection of Aerofoil based on Flow Induced Vibration and Damping Ratio", IJSDR - International Journal of Scientific Development and Research (www.IJSDR.org), ISSN:2455-2631, Vol.2, Issue 7, page no.258 - 263, July-2017, Available :https://ijsdr.org/papers/IJSDR1707041.pdf
Volume 2
Issue 7,
July-2017
Pages : 258 - 263
Paper Reg. ID: IJSDR_170642
Published Paper Id: IJSDR1707041
Downloads: 000347257
Research Area: Engineering
Country: Theni, Tamil Nadu, India
ISSN: 2455-2631 | IMPACT FACTOR: 9.15 Calculated By Google Scholar | ESTD YEAR: 2016
An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 9.15 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator
Publisher: IJSDR(IJ Publication) Janvi Wave
