Programming a Multiple-Orifice Hydraulic Decelerator.

Abstract

The AAMRL Horizontal Deceleration Facility is used to conduct experimental research for the development of design criteria for aircrew personnel protection. The hydraulic deceleration device is a water-filled cylinder. A piston mounted on the front of a deceleration sled ruptures a frangible diaphragm positioned at the opening of the cylinder and displaces the water in the cylinder through the multiple orifices. As the piston travels along the cylinder it closes off the orifices thereby decreasing the available area for the water to escape. Bernoulli's conservation-of-energy equation was applied to the physical state of fluid flow in the cylinder, allowing the orifice area to be determined as a function of the piston cross-sectional area, acceleration, velocity and weight of the sled. A computer program was developed to determine the appropriate plug orifice and location to produce desired acceleration-time profiles. The program corrects for the energy loss due to the vena-contracta of each plug. Data from several tests were used to determine a correction coefficient for other losses, such as those attributable to conduit length and surface roughness, as a lumped quantity. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1985
Accession Number
ADA159428

Entities

People

  • C. G. Toler

Organizations

  • Armstrong Laboratory

Tags

Communities of Interest

  • Biomedical
  • Human Systems
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Back Pressure
  • Biomedical Research
  • Classification
  • Computer Programming
  • Computer Programs
  • Corporations
  • Deceleration
  • Design Criteria
  • Dynamic Response
  • Equations
  • Flow
  • Fluid Flow
  • Impact Tests
  • Security
  • Test Facilities

Readers

  • Combustion and Flow Dynamics.
  • Electrical Engineering
  • Explosive Engineering.