AERODYNAMIC RESISTANCE OF SMOOTH-PIPE STAGGERED BUNDLES IN A CROSS FLOW OF AIR AT HIGH RE NUMBERS,

Abstract

An experimental investigation was made of the resistance of five smooth-pipe staggered bundles a/b = 1.27 -1.94 in a cross flow of air in the interval Re of from 10,000 to 2,000,000. The dependence of the resistance of the bundles on the number of longitudinal rows z2 was investigated. It was established that the character of the resistance stabilizes at seven longitudinal rows and does not depend on further increase in the number of them. The results were evaluated in criterial form and the graphic dependences are given. Analysis of the material obtained showed that in the region Re = (1.8--1.6) x 100,000 there begins the transition into the self-modeling zone of developed turbulence. In close-staggered bundles (a/b< or =1.7), the self-modeling zone occurs immediately, but in less close ones (a/b>1.7) the automatic operation sets in after the transition zone. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 22, 1965
Accession Number
AD0622464

Entities

People

  • P. S. Samoshka
  • Yu. K. Stasyulyavichyus

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Automatic
  • Cross Flow
  • Flow
  • Intervals
  • Materials
  • Personality
  • Resistance
  • Transitions
  • Turbulence

Fields of Study

  • Engineering

Readers

  • Combustion and Flow Dynamics.