FREE-FIELD PRESSURES, STATION ZERO

Abstract

Free-field pressures as a function of time were measured at eight positions above the Wigwam weapon at distances from the charge varying from 800 to 1975 ft. Tourmaline PE gauges were used. Signals were either telemetered to a remote receiving location or were recorded in place on a magnetic-tape recorder that was recovered after the shot. The variation of maximum observed pressure in pounds per square inch with distance in feet from the weapon in this range is given by the expression P(max) 2.03 x 10 to the 7th power/R to the 1.16th power. Impulse, at locations not affected by surface cutoff, is given by the expression I 3.36 x 10,000/R to the .77th power where I is in pound seconds per square inch. Energy flux density, at locations not affected by surface cutoff, is given by the expression E 3.81 x 10 to the 10th power/R to the 1.87th power where E is in inch pounds per square inch. The fiducial pulse was recorded at 12.5 = 1 msec be fore weapon detonation. The shock wave arrived at the water surface 385.5 msec after the fiducial pulse. The equivalent weight of TNT required to produce the same peak pressures as the Wigwam weapon at 2000 ft was 4.05 x 10 to the 7th power lb.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1955
Accession Number
AD0339495

Entities

People

  • C. B. Cunningham

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Biomedical
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Energy Systems
  • Engineering
  • Explosions
  • Flux Density
  • Frequency Response
  • Generators
  • Measurement
  • Measuring Instruments
  • Munitions
  • Nuclear Energy
  • Ordnance Laboratories
  • Recording Systems
  • Tape Recorders
  • Tape Recording
  • Telemetering Transmitters
  • Telemetry Equipment
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Computer Science/Computer Engineering/Data Science/Digital Signal Processing.
  • Explosive Engineering.
  • Regression Analysis.