Vortex Sensing Tests at NAFEC.

Abstract

The report describes the results of a series of tests to determine and evaluate three experimental techniques for remote sensing of the wing-tip vortices generated by heavy commercial and military aircraft. These techniques involved a pulsed, bistatic acoustic detection and ranging system (referred to as an acoustic radar); a ground level pressure sensor, and a ground level hot-wire anemometer. Results in the form of altitudes and times of tower hits and vortex tracks are presented and compared to the tower data wherever possible.

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1972
Accession Number
AD0749908

Entities

People

  • D. Burnham
  • J. Hallock
  • R. Kodis
  • T. Sullivan

Organizations

  • John A. Volpe National Transportation Systems Center

Tags

Communities of Interest

  • Sensors

DTIC Thesaurus Topics

  • Acoustic Detection
  • Aircrafts
  • Anemometers
  • Detection
  • Detectors
  • Ground Level
  • Hot Wire
  • Hot Wire Anemometers
  • Military Aircraft
  • Range Finding
  • Remote Sensing
  • Sodar
  • Wing Tips

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation
  • Fluid Dynamics.
  • Radar Systems Engineering.