NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Testing superalloys at 2000 (1367) and 2200 F (1478 K) in a Mach 4.6 airstreamSeven superalloy models were tested in a plasma arc tunnel facility. The test models were 3 in. (7.62cm) square flat surfaces (nominally 0.01 to 0.02 in. (0.0254 to 0.0508 cm) thick) held in a water-cooled wedge holder at a 60 deg (1.05 rad) angle of attack. The models were cycled 25 times (two were cycled 50 times) for 10 min each cycle in a Mach 4.6 test stream with the model leading edge temperature maintained at 2200 F (1478 K) (one at 2000 F (1367 K)). Backface temperatures were measured with four platinum-platinum 10% rhodium thermocouples and the front surface temperatures with an optical pyrometer. Four different nickel base alloy materials and one cobalt material were evaluated.
Document ID
19720018790
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Land, D. W.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Williams, R. R.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Rinehart, W. A.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1972
Subject Category
Materials, Metallic
Report/Patent Number
MDC-Q0449
NASA-CR-120913
Report Number: MDC-Q0449
Report Number: NASA-CR-120913
Accession Number
72N26440
Funding Number(s)
CONTRACT_GRANT: NAS3-14666-H
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available