Impedance of Asymmetrically-Fed Trailing-Wire Antennas

Abstract

The paper considers the impedance of long wires towed by aircraft for low-frequency communications. Experiments using a small helicopter towing wires up to 1850 feet in length are described. The effects of wire slenderness factor (l/a) and r-f ohmic resistance on efficiency and input impedance are considered. Particular attention is devoted to the synthesis of a model which can be used to predict the impedance of trailing wires for any wire length and aircraft size. It is concluded that wires several miles long towed by aircraft need not be excited at their centers, but can be conveniently and efficiently driven from the aircraft.

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Document Details

Document Type
Technical Report
Publication Date
Mar 22, 1962
Accession Number
AD0731777

Entities

People

  • W. E. Buehler

Organizations

  • Boeing

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Airplanes
  • Antennas
  • Capacitance
  • Cylindrical Antennas
  • Electric Fields
  • Equivalent Circuits
  • Frequency
  • Ground Effect
  • Helicopters
  • Impedance
  • Measurement
  • Q Meters
  • Trailing Wire Antennas
  • Transport Aircraft

Readers

  • Aerospace Engineering
  • Electromagnetic Wave Scattering and Antenna Radiation Engineering
  • Marine Hydrodynamics