Author details

Jaeha Ryi\* and Jong-Soo Choi

\*Address all correspondence to: bass83@cnu.ac.kr

Department of Aerospace Engineering, Chungnam National University, Daejeon, Korea

test [the Degree of Ph.D.]. Department of Aerospace Engineering, Chungnam National

Estimation Method to Achieve a Noise Reduction Effect of Airfoil with a Serrated Trailing Edge for Wind…

http://dx.doi.org/10.5772/intechopen.73608

145

[11] Brooks TF, Marcolini MA. Airfoil trailing edge flow measurements and comparisøn with theory incorporating open wind tunnel corrections. In: AIAA-84-2266, AIAA/NASA 9th

[12] Garner HC, Rogers EWE, Acum WEA, Maskell EC. Subsonic Wind Tunnel Wall Correc-

[13] Brooks T, Pope D, Marcolini M. Airfoil Self-Noise and Prediction, NASA Reference

[14] Brooks TF, Marcolini MA. Airfoil tip vortex formation noise. AIAA Journal. Feb. 1986;

University; Feb. 2015

Aeroacoustic Conference; 1984

tions. NATO, AGARD; 1966

Publication 1218; 1989

24(2):246-252
