NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
NTF model concept for the X-29A. Part 1: Requirements, guidelines, and design loadsA few Charpy samples containing a transverse EB weld at the V-notch location were produced. Three tensile specimens containing a transverse weld were also produced. These samples were tested at cryogenic temperatures. The welded Charpy samples resulted in average impact values of 20 ft-lb. This average value is as good as the NASA test samples with the base metal. The tensile specimens broke at slightly higher loads than had been calculated. The Charpy specimens did not come up to the prescribed level of 25 ft-lb. The results of the specimen tests are presented.
Document ID
19830010485
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Daforno, G.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1983
Publication Information
Publication: NASA. Langley Research Center Cryogenic Wind Tunnel Models
Subject Category
Research And Support Facilities (Air)
Accession Number
83N18756
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available