Unsteady Lift Model for Morphing Airfoil Based on Potential Flow Theory-Reference-Cited by-同舟云学术

Unsteady Lift Model for Morphing Airfoil Based on Potential Flow Theory

Published:2018-03 Issue:2 Volume:31 Page:04018006
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Li Shaobin¹,Tao Zhenxin²,Song Xizhen³

Affiliation:

1. Lecturer, School of Energy and Power Engineering, Beihang Univ., Beijing 100191, China (corresponding author).

2. Master, Hunan Aviation Powerplant Research Institute, Aero Engine (Group) Corporation of China, Zhuzhou 412000, China.

3. Lecturer, School of Energy and Power Engineering, Beihang Univ., Beijing 100191, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000820

Reference25 articles.

1. Ai Q. Jawahar H. K. and Azarpeyvand M. (2016). “Experimental investigation of aerodynamic performance of airfoils fitted with morphing trailing edges.” 54th AIAA Aerospace Sciences Meeting AIAA Reston VA.

2. A Review of Morphing Aircraft

3. The relationship between 3-D kinematics and gliding performance in the southern flying squirrel, Glaucomys volans

4. Bowman J. Sanders B. and Weisshaar T. (2002). “Evaluating the impact of morphing technologies on aircraft performance.” 43rd AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Materials Conf. Structures Structural Dynamics and Materials and Co-Located Conf. AIAA Reston VA.

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