Dye Visualization of the Vortical Flow Structure over a Double-Delta Wing

Author:

Thu Aung Myo1,Byun Yung Hwan2,Lee Jae-Woo3

Affiliation:

1. Doctoral Fellow, Dept. of Aerospace Information Engineering, Konkuk Univ., 1 Hwayang-dong, Gwangjin-gu, Seoul 143-701, Korea.

2. Professor, Dept. of Aerospace Information Engineering, Konkuk Univ., 1 Hwayang-dong, Gwangjin-gu, Seoul 143-701, Korea (corresponding author).

3. Professor, Dept. of Aerospace Information Engineering, Konkuk Univ., 1 Hwayang-dong, Gwangjin-gu, Seoul 143-701, Korea.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference16 articles.

1. Brennenstuhl U. (1985). “Experimentelle und theoretische untersuchungen uber die wirbelbildung an doppeldeltaflugeln.” Ph.D. dissertation Carola Wilhelmina Technical Univ. Braunschweig Germany.

2. Low-speed unsteady aerodynamics of a pitching straked wing at high incidence-Part II: Harmonic analysis

3. Erickson G. E. (1980). “Flow studies of slender wing vortices.” 13th Fluid and Plasma Dynamics Conf. American Institute of Aeronautics and Astronautics Washington DC.

4. Frink N. T. and Lamar J. E. (1980). “Water-tunnel and analytical investigation of the effect of strake design variables on strake vortex breakdown characteristics.” NASA TP 1676 National Aeronautics and Space Administration Washington DC.

5. Gai S. L. Roberts M. Barker A. Kleczaj C. and Riley A. J. (2004). “Vortex interaction and breakdown over double-delta wings.” Aeronaut. J. 108(1079) 27–34.

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