The Drag of Projectiles with Truncated Cone Headshapes

Abstract

A series of projectiles with truncated conical headshapes (24 deg 12 min included cone angle) were fired in the Aerodynamics Range and their drag was determined from time measurements and spark photographic records of distance. The drag was found to increase linearly with meplat diameters except for small meplats. A comparison was made with pointed cone head projectiles of the same head lengths as the truncated series, the drags of the pointed projectiles being estimated from the measured drag of the 24 deg 12 min complete cone projectile. The drag of the truncated cone projectiles is lower throughout at Mach number 1. 65 and for meplat diameters to 0.4 calibers at M 2.35.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1952
Accession Number
AD0800468

Entities

People

  • A. C. Charters
  • H. Stein

Organizations

  • Ballistic Research Laboratory

Tags

DTIC Thesaurus Topics

  • Base Pressure
  • Bodies
  • Boundary Layer
  • Cylindrical Bodies
  • Diameters
  • Drag
  • Flow
  • Friction
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Projectiles
  • Shock Waves
  • Skin Friction
  • Stagnation Pressure
  • Trajectories

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.