Flutter Instability of a Fluid-Conveying Fluid-Immersed Pipe Affixed to a Rigid Body

Abstract

A set of simplified boundary conditions for a flexible beam connected to a rigid body at one end and free at the other end is presented and applied to the case of a fluid-conveying, fluid-immersed pipe. These boundary conditions represent an analytically tractable approximation to those of a submersible which uses a combination of jet action and flutter instability induced tail motion to produce thrust. The boundary conditions are made non-dimensional, and the effect of the non-dimensional mass of the rigid body on system stability is assessed. The neutral stability of this system is determined within a two-parameter space consisting of the velocity of the fluid within the tail, and the forward speed of the submersible. Equations in the literature, derived using slender-body theory, were used to compute the sign of the thrust produced by the tail and the tail's Froude efficiency for the neutrally stable waveforms of the beam.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 2011
Accession Number
ADA549327

Entities

People

  • Andrew John Hull
  • Aren Hellum
  • Ranjan Mukherjee

Organizations

  • Naval Undersea Warfare Center

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Axial Flow
  • Boundaries
  • Civil Engineering
  • Computational Science
  • Engineering
  • Equations
  • Equations Of Motion
  • Fluid Mechanics
  • Frequency
  • Geometry
  • Instability
  • Mechanical Engineering
  • Mechanics
  • Payload
  • Phase Velocity
  • Slender Bodies
  • United States

Fields of Study

  • Mathematics

Readers

  • Fluid Dynamics.
  • Marine Hydrodynamics
  • Structural Dynamics.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster
  • Space - Spacecraft Maneuvers