The Use of Bonded Rubber Pads for the Application of Loads for Structural Testing of the P-3 Orion Leading Edge.
Abstract
Aerodynamic loads on aircraft lifting surfaces are often due to negative pressures acting on the outer skin of the structure. To simulate this type of loading, rubber pads bonded to the skin and loaded in tension can be used. This report describes the development of a contact adhesive based bonded rubber tension pad system for testing of an Orion P-3 wing leading edge.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1997
- Accession Number
- ADA329920
Entities
People
- G. Luke
- T.j. Van Blaricum
Organizations
- Defence Science and Technology Group