Optimal Placement of Non-Intrusive Waste Heat Recovery Devices in Exhaust Ducts

Abstract

The Secretary of the Navy has ordered the U.S. Navy and Marine Corps to reduce energy usage. This study explores how to optimize placement and size of a non-intrusive waste heat recovery device for energy recovery in exhaust ducts. Additionally, it explores the effect that a device has on the exhaust infrared signature by analyzing the change in the bulk temperature at the exhaust outlet. Optimal device placement and size is dependent on duct geometry, external heat transfer coefficient, and flow characteristics, namely Reynolds number. Infrared signature intensity reductions of 1 14% are only achievable with unpractically long thermoelectric generator devices and high external heat transfer coefficients. Doubling the external heat transfer coefficient increases heat recovery by 15 30% for low Reynolds number flows (104) and 75 90% for high Reynolds number flows (105~106). In low Reynolds number flows (~104), device position can account for a 75% change in energy recovery whereas high Reynolds number flows (~106) have unexpected areas of higher heat transfer. Position changes can increase heat recovery 10 70%, while increasing device size may only marginally improve results. Identifying local maxima for heat transfer, especially in high Reynolds number flows (~106), is counterintuitive because of unexpected recirculation zone effects.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 2015
Accession Number
ADA632282

Entities

People

  • Ryan S. Bohning

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Boundary Layer
  • Climate Change Adaptation
  • Computational Fluid Dynamics
  • Energy
  • Energy Storage
  • Energy Transfer
  • Fluid Dynamics
  • Fluid Flow
  • Heat Energy
  • Heat Recovery
  • Heat Transfer
  • Heat Transfer Coefficients
  • Mechanical Engineering
  • Specific Heat
  • Three Dimensional
  • Turbines
  • Two Dimensional

Readers

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  • Fluid Dynamics.
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