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Experimental Investigation on the Dynamic Characteristics of a Concentric Membrane Tank

Research Project

Project/Area Number 16560693
Research Category

Grant-in-Aid for Scientific Research (C)

Allocation TypeSingle-year Grants
Section一般
Research Field Aerospace engineering
Research InstitutionJapan Aerospace Exploration Agency

Principal Investigator

KOMATSU Keiji  Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science Department of Space Structure and Materials, 宇宙科学研究本部宇宙構造・材料工学研究系, 教授 (20358683)

Project Period (FY) 2004 – 2006
Project Status Completed (Fiscal Year 2006)
Budget Amount *help
¥3,600,000 (Direct Cost: ¥3,600,000)
Fiscal Year 2006: ¥400,000 (Direct Cost: ¥400,000)
Fiscal Year 2005: ¥200,000 (Direct Cost: ¥200,000)
Fiscal Year 2004: ¥3,000,000 (Direct Cost: ¥3,000,000)
Keywordssloshing / vibration / membrane / tank / concentric / hydroelasticity / shell / rocket / 液体 / 減衰
Research Abstract

Sloshing describes the free-surface oscillations of a liquid in a partially filled tank, which results from lateral and longitudinal displacements or angular motions of the vehicle containing the liquid. A concentric membrane tank configuration is a possible design concept for reducing the structural weight of a launch vehicle. Due to the geometrical arrangement and flexibility of the inner tank, attitude control and propulsion system stability margins may be changed in comparison with those of the conventional tandem tank configuration.
In this research, we experimentally investigated the dynamic characteristics of the lateral liquid sloshing in a concentric tank from the view-point of attitude stability and control. We conducted an experiment using a circular cylindrical tank having a rigid outer wall of 33.4-cm diameter and a flexible inner wall of 23.4-cm diameter. The three materials used for the inner walls were, rigid acrylic, Kapton film, and polyethylene foam sheeting.
We found that in the membrane wall, the outer part resonant phenomenon was difficult to clearly discern, because of the heavy motion coupling of the inner and outer liquids through the flexible membrane wall. Consequently the apparent damping ratio was increased with decreasing rigidity of the membrane wall.

Report

(4 results)
  • 2006 Annual Research Report   Final Research Report Summary
  • 2005 Annual Research Report
  • 2004 Annual Research Report

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Published: 2004-04-01   Modified: 2016-04-21  

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