Adaptive Control of Shock Waves with a Passively Morphing Layer for Rotating Blades

Author:

Shi Junxiang1,Xu Tiancheng2,Schafer Steven R.3,Chen Chung-Lung4

Affiliation:

1. Postdoctoral Researcher, Dept. of Mechanical and Aerospace, Univ. of Missouri-Columbia, Columbia, MO 65211.

2. Graduate Student, Dept. of Mechanical and Aerospace, Univ. of Missouri-Columbia, Columbia, MO 65211.

3. Undergraduate Student, Dept. of Mechanical and Aerospace, Univ. of Missouri-Columbia, Columbia, MO 65211.

4. Professor, Dept. of Mechanical and Aerospace, Univ. of Missouri-Columbia, Columbia, MO 65211 (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Reference30 articles.

1. ANSYS version 14.0 [Computer software]. Canonsburg PA ANSYS Inc.

2. Modeling of Controlled Shock-Wave/Boundary-Layer Interactions in Transonic Channel Flow

3. Shock control on a swept wing

4. Bousman W. G. (2002). “Airfoil design and rotorcraft performance.” American Helicopter Society 58th Annual Forum.

5. Aerodynamic Characteristics of SC1095 and SC1094 R8 Airfoils

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