RADAR STUDY OF SPHERE WAKES

Abstract

A series of firings was executed in the 100-ft Range K of the VKF for the purpose of determining the causes of radar reflections from the wakes of hypervelocity spheres. A 35-kmc, focused, oblique radar was employed as the primary instrumentation. In addition, receiving and parasite antennas were used to measure transmission and specular reflection. The results of these experiments indicate that, when using the 35-kmc microwave equipment described here, a detectable radar reflection in most cases was obtained from the wake of a hypervelocity sphere (10,000 to 27,000 ft/sec in these experiments) only if the sphere ablated. Measurements of turbulent wake velocity were shown to agree with the predicted values. The region of transition from laminar to turbulent flow was also defined.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1966
Accession Number
AD0802526

Entities

People

  • A. B. Bailey
  • R. E. Hendrix

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Attenuation
  • Doppler Radar
  • Engineering
  • Flow
  • Frequency
  • Frequency Shift
  • Government (Foreign)
  • Governments
  • Instrumentation
  • Materials
  • Measurement
  • Microwave Equipment
  • Radar
  • Stagnation Point
  • Turbulent Mixing

Fields of Study

  • Physics

Readers

  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Fluid Dynamics.
  • Fluid Mechanics and Fluid Dynamics.

Technology Areas

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