Influence of Geometric Coupling on the Whirl Flutter Stability in Tiltrotor Aircraft with Unsteady Aerodynamics-Reference-Cited by-同舟云学术

Influence of Geometric Coupling on the Whirl Flutter Stability in Tiltrotor Aircraft with Unsteady Aerodynamics

Published:2012-01 Issue:1 Volume:25 Page:143-148
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Kim Taeseong¹²³,Shin SangJoon¹²³,Kim Do-Hyung¹²³

Affiliation:

1. Research Scientist, Wind Energy Division, Building 118, Risø DTU, Roskilde, 4000, Denmark.

2. Associate Professor, Institute of Advanced Aerospace Technology, School of Mechanical and Aerospace Engineering, Building 301, Room 1418, Seoul National Univ., Seoul, 151-742, Korea (corresponding author).

3. Research Engineer, Rotor Dept., Korea Aerospace Research Institute, 45 Eoeun-dong, Yuseong-gu, Daejeon, 305-333, 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%29AS.1943-5525.0000096

Reference31 articles.

1. Bauchau O. A. (2006). “DYMORE user’s manual.” School of Aerospace Engineering Georgia Institute of Technology Atlanta.

2. Bell Helicopter. (1971). “Advancement of proprotor technology task. II: Wind-tunnel test results.” NASA CR 114363 Bell Helicopter Co. Fort Worth TX.

3. DeLarm L. (1969). “Whirl flutter and divergence aspects of tilt-wing and tilt-rotor aircraft.” Proc. U.S. Air Force V/STOL Technology Planning Conf. Air Force Flight Dynamics Laboratory Air Force Systems Command Wright-Patterson Air Force Base Dayton OH.

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