Nonlinear Aeroelastic Simulation of a Full-Span Aircraft with Oscillating Control Surfaces-Reference-Cited by-同舟云学术

Nonlinear Aeroelastic Simulation of a Full-Span Aircraft with Oscillating Control Surfaces

Published:2005-07 Issue:3 Volume:18 Page:156-167
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yoo Jae-Han¹²³⁴,Kim Dong-Hyun¹²³⁴,Kwon Hyuk-Jun¹²³⁴,Lee In¹²³⁴

Affiliation:

1. Graduate Research Assistant, Dept. of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST), 373-1 Guseong-dong, Yuseong-gu, Daejeon, 305-701, Republic of Korea.

2. Assistant Professor, School of Mechanical and Aerospace Engineering (with ReCAPT), Gyeongsang National Univ. (GSNU), 900 Gazwa-dong, Jinju, Kyungnam, 660-701, Republic of Korea.

3. Graduate Research Assistant, Dept. of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST), 373-1 Kusong-dong, Yusong-gu, Taejon, 305-701, Republic of Korea.

4. Professor, Dept. of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST), 373-1 Kusong-dong, Yusong-gu, Taejon, 305-701, Republic of Korea.

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%290893-1321%282005%2918%3A3%28156%29

Reference9 articles.

1. Wing flutter boundary prediction using unsteady Euler aerodynamic method

2. Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations

3. Unsteady transonic flow calculations for realistic aircraft configurations

4. Wing-flutter calculations with the CAP-TSD unsteady transonic small-disturbance program

5. Unsteady transonic aerodynamics and aeroelastic calculations at low-supersonic freestreams

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