Hydrodynamic Ram Simulator

Abstract

The objective of this work was to develop a low-cost method of evaluating hydrodynamic ram and blast effects on aircraft materials that is effective for both joint and flat plate testing and able to assess failure properties of both types of structures. The approach was to revise the design of the RamGun test device to avoid previously discovered shortfalls. This was to be done as follows: 1.)Larger test section to avoid boundary effects,2.) Elimination of internal reflections that confound data, 3.)Tuned pressure pulses that map to specific threats, 4.)Design supported by LSDYNA, 5.)Dem-val tests to verify final design. The effort was piggy-backed onto a Phase II SBIR. The focus of this report is the design support being performed by LSDYNA simulations in support of the SBIR tasks.

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Document Details

Document Type
Technical Report
Publication Date
Sep 30, 2008
Accession Number
ADA490882

Entities

People

  • Albert Moussa
  • Gangming Zhang
  • Ronald Hinrichsen
  • Stephen Stratton

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Guns
  • Aircrafts
  • Airframes
  • Blast
  • Boundaries
  • Cargo Aircraft
  • Concept 1
  • Fighter Aircraft
  • Kinetic Energy
  • Materials
  • Reflection
  • Simulations
  • Test Methods
  • Three Dimensional
  • Transport Aircraft
  • Water Tanks

Readers

  • Nanoscale Plasmonic Nanotechnology
  • Software Engineering
  • Systems Analysis and Design