FACTORS EFFECTING THE DESIGN OF A SYSTEM FOR TOWING A BODY ON A LONG LENGTH OF WIRE

Abstract

A method of calculating the diameter of wire to be used and the drag area of target to be towed in order to meet a given requirement of maximum speed of towing and maximum length of tow is presented. Particular reference is made to a towed target system of the Del Mar Company of Los Angeles U.S.A. and further analysis is made of U.S. Air Force test data on this system. The test data, despite not having been obtained in a fully controlled scientific experiment, is the best so far known for evaluating the skin drag coefficients of piano wire and predicts a variation both with air speed and with wire diameter. Analysis predicts that there is a region at high subsonic airspeed and at medium altitudes where the towed system can become unstable.

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1962
Accession Number
AD0296137

Entities

People

  • G. W. Stevens

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Altitude
  • Design Criteria
  • Drag
  • Equations
  • Government Procurement
  • High Altitude
  • Instability
  • Materials
  • Measurement
  • Medium Altitude
  • Standards
  • Towed Bodies
  • Towed Targets

Fields of Study

  • Engineering
  • Physics

Readers

  • Computational Modeling and Simulation
  • Electrical Engineering
  • Marine Hydrodynamics