Hypersonic and Unsteady Flow Science Issues for Explosively Formed Penetrator Warheads

Abstract

The technology of hypersonic projectiles is becoming mature from a metal physics perspective but there are still unsolved challenges relating to flight characteristics and aerodynamic stability. These projectiles deform under explosive loads and accelerate to hypersonic speeds in 2x10-6 seconds. In addition, these projectiles operate at sea-level conditions, a high-speed flight regime not commonly studied. The objective of this effort is to study the aerodynamics characteristics of deformable projectiles flying at hypersonic speeds and sea-level conditions. Because aerodynamic stability is critical for proper performance it is important to know what shapes should be avoided and which ones are acceptable. Since this was a short one-year IDP task the effort only focused on static body geometries, no deformable body calculations were attempted.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 2006
Accession Number
ADA452661

Entities

People

  • Ben Case
  • Jacobs Sverdrup
  • Kirk Vanden
  • Steve Ellison

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Stability
  • Air Force
  • Air Force Research Laboratories
  • Aircrafts
  • Boundary Layer
  • Chemical Reactions
  • Computational Fluid Dynamics
  • Computational Mechanics
  • Explosively Formed Penetrators
  • Explosives
  • Flow Fields
  • Mechanics
  • Military Research
  • Munitions
  • Penetrator Warheads
  • Sea Level
  • Unsteady Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Defense Technology Research and Development.
  • Explosive Engineering.

Technology Areas

  • Hypersonics