National Technical Reports Library - NTRL

National Technical Reports Library

The National Technical Information Service acquires, indexes, abstracts, and archives the largest collection of U.S. government-sponsored technical reports in existence. The NTRL offers online, free and open access to these authenticated government technical reports. Technical reports and documents in its repository may be available online for free either from the issuing federal agency, the U.S. Government Publishing Office’s Federal Digital System website, or through search engines.




Details
Actions:
Download PDFDownload XML
Download

Heat and Momentum Transfer to Internal Turbulent Flow of Helium-Argon Mixtures in Circular Tubes. Revision.


ADA167290

Publication Date 1978
Personal Author Pickett, P. E.
Page Count 128
Abstract Experimental results of an investigation of friction and heat transfer parameters for turbulent flow of helium-argon (He-A) mixtures in smooth, electrically heated, circular tubes are compared to existing experimental correlations and to analytical results. He-A mixtures with molecular weights between 15.3 and 29.7 are used, resulting in Prandtl numbers between 0.42 and 0.49. Inlet Reynolds numbers range from 31200 to 102000, maximum wall temperatures from 392 to 828 k, maximum wall-to-bulk temperature ratios to 1.82, maximum wall heat flux values to 511 KW/ sq m, and pressures from 469 to 967KPa. Existing experimental correlations, developed using gases with Prandtl numbers of approx. 0.7, are compared to the measured friction and heat transfer results. Adiabatic friction factors and friction factors with heat addition are predicted with + or - 4 and + or - 10 percent, respectively. Nusslt numbers for fully developed, constant property conditions are predicted within + or - 5.0 %. An empirical equation that correlates the He-A data within + or - 15% and includes entrance and variable property effects is presented. Keywords: Boundary layer, Forced convection; Brayton cycles; heat exchangers; Noble gas mixtures; Gas turbine cycles.
Keywords
  • Brayton cycle
  • Gas turbines
  • Heat exchangers
  • Turbulent flow
  • Convection(Heat transfer)
  • Addition
  • Adiabatic conditions
  • Argon
  • Boundary layer
  • Convection
  • Equations
  • Friction
  • Heat
  • Heat transfer
  • Helium
  • Inlets
  • Mixtures
  • Momentum transfer
  • Prandtl number
  • Reynolds number
  • Tubes
  • Circular
  • Thermal properties
Source Agency
  • Non Paid ADAS
NTIS Subject Category
  • 46 - Physics
  • 81D - Jet & Gas Turbine Engines
Corporate Authors Arizona Univ., Tucson. Engineering Experiment Station.
Document Type Technical Report
Title Note Interim rept.
NTIS Issue Number 198617
Contract Number
  • N00014-75-C-0694
Heat and Momentum Transfer to Internal Turbulent Flow of Helium-Argon Mixtures in Circular Tubes. Revision.
Heat and Momentum Transfer to Internal Turbulent Flow of Helium-Argon Mixtures in Circular Tubes. Revision.
ADA167290

  • Brayton cycle
  • Gas turbines
  • Heat exchangers
  • Turbulent flow
  • Convection(Heat transfer)
  • Addition
  • Adiabatic conditions
  • Argon
  • Boundary layer
  • Convection
  • Equations
  • Friction
  • Heat
  • Heat transfer
  • Helium
  • Inlets
  • Mixtures
  • Momentum transfer
  • Prandtl number
  • Reynolds number
  • Tubes
  • Circular
  • Thermal properties
  • Non Paid ADAS
  • 46 - Physics
  • 81D - Jet & Gas Turbine Engines
  • N00014-75-C-0694
Loading