MILES Pressure/Seismic Response-Initial Study and Analysis.
Abstract
This is an initial study and analysis of a method for testing the pressure/seismic response of a MILES transducer. The testing approach described is based on an experimentally verified mathematical model for the line transducer. A preliminary design for a test apparatus and a test procedure not only evaluates the pressure/seismic response, but also develops all additional data required for acceptance testing of a MILES transducer. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1977
- Accession Number
- ADA042095
Entities
People
- B. E. Barnes
- J. B. Starr
- M. R. Ludwig
Organizations
- Honeywell International, Inc.