High-Lift Effect of Bionic Slat Based on Owl Wing

Author:

Ge Changjiang,Ren Luquan,Liang Ping,Zhang Chengchun,Zhang Zhihui

Publisher

Springer Science and Business Media LLC

Subject

Bioengineering,Biophysics,Biotechnology

Reference19 articles.

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2. Soderman P T, Kafyeke F, Boudreau J, Burnside N J, Jaeger S M, Chandrasekharan R. Airframe noise study of a Bombardier CRJ-700 aircraft model in the NASA Ames 7- by 10-foot wind tunnel. International Journal of Aeroacoustics, 2004, 3, 1–42.

3. Chow L C, Mau K, Remy H. Landing gear and high lift devices airframe noise research. AIAA Paper, 2002, 2002–2408.

4. Ma Z K. Slat noise attenuation using acoustic liner. AIAA Paper, 2005, 2005–3009.

5. Smith M G, Chow L C, Molin N. Attenuation of slat trailing edge noise using slat gap acoustic liners. AIAA Paper, 2006, 2006–2666.

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