NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Demonstration test of burner liner strain measurement systems: Interim resultsWork is in progress to demonstrate two techniques for static strain measurements on a jet engine burner liner. Measurements are being made with a set of resistance strain gages made from Kanthal A-1 wire and via heterodyne speckle photogrammetry. The background of the program is presented along with current results.
Document ID
19860002034
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stetson, K. A. (United Technologies Research Center East Hartford, CT, United States)
Grant, H. P. (Pratt and Whitney Aircraft East Hartford, Conn., United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1983
Publication Information
Publication: NASA. Lewis Research Center Turbine Eng. Hot Sect. Technol. (HOST)
Subject Category
Structural Mechanics
Accession Number
86N11501
Funding Number(s)
CONTRACT_GRANT: NAS3-23690
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19860002028Collected WorksTurbine Engine Hot Section Technology (HOST)19860002028Collected WorksTurbine Engine Hot Section Technology (HOST)
No Preview Available