Effect of Fuel Sloshing in the External Tank on the Flutter of Subsonic Wings-Reference-Cited by-同舟云学术

Effect of Fuel Sloshing in the External Tank on the Flutter of Subsonic Wings

Published:2014-09 Issue:5 Volume:27 Page:04014021
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Firouz-Abadi R. D.¹,Zarifian P.²,Haddadpour H.³

Affiliation:

1. Assistant Professor, Dept. of Aerospace Engineering, Sharif Univ. of Technology, P.O. Box 11155-8639, Tehran, Iran (corresponding author).

2. Research Fellow, Dept. of Aerospace Engineering, Sharif Univ. of Technology, P.O. Box 11155-8639, Tehran, Iran.

3. Professor, Dept. of Aerospace Engineering, Sharif Univ. of Technology, P.O. Box 11155-8639, Tehran, Iran.

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.1943-5525.0000261

Reference22 articles.

1. Abramson H. N. (1966). “The dynamic behavior of liquids in moving containers.” Nasa sp–106 NASA Washington DC.

2. Studies of Store-Induced Limit-Cycle Oscillations Using a Model with Full System Nonlinearities

3. Dynamic Aeroelastic Instabilities of an Aircraft Wing with Underwing Store in Transonic Regime

4. Chiu E.-Y. and Farhat C. (2009). “Effects of fuel slosh on flutter prediction.” 50th AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Materials Conf.

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