HYPERSONIC STUDIES OF WAKES BEHIND CYLINDERS. PART I: PITOT PRESSURE MEASUREMENTS AT M = 16 IN HELIUM,

Abstract

The pitot pressure was measured in the wake of two-dimensional circular cylinders at a Mach number of 16 in helium. The diameters of the cylinders used were 1/8 inch and 3/16 inch giving a Reynolds number variation of 10,500 to 25,300 based on free stream conditions. Surveys were performed as far back as 80 body diameters. Profiles in the far wake at the same x/D were similar, independent of body Reynolds number. The wake growth was found to vary as the 0.6 power. Body Reynolds number had no effect on the rate of growth over the range studied. It was not possible to deduce transition from the pitot pressure measurement alone. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1965
Accession Number
AD0467691

Entities

People

  • I. E. Vas
  • J. D. Ledger
  • S. M. Bogdonoff

Organizations

  • Princeton University

Tags

DTIC Thesaurus Topics

  • Diameters
  • Free Stream
  • Mach Number
  • Measurement
  • Physical Properties
  • Pressure Measurement
  • Reynolds Number
  • Transitions
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow