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There are a total of 10 record(s) matching your query.
Sorted by: Date Added To NTRS in Descending order
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Structural analyses of engine wall cooling concepts and materials
Author(s): Kaufman, Albert
Abstract: The severe thermal environments under which hypersonic aircraft such as the National Aerospace Plane (NASP) will operate require cooling of the engine walls, especially in the combustor. A preliminary assessment is made of ...
NASA Center: NASA (non Center Specific) Publication Year: 1988
Added to NTRS: 2008-05-30
Accession Number: 88N22405; Document ID: 19880013021
The design of brittle-material blade roots based on theory and rupture tests of plastic models
Author(s): Meyer, Andre J , Jr; Kaufman, Albert; Caywood, William C
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1953
Added to NTRS: 2006-11-06
Accession Number: 93R17059; Document ID: 19930087769; Report Number: NACA-RM-E53C12
Comparative tensile strengths at 1200 F of various root designs for cermet turbine blades
Author(s): Meyer, Andre J , Jr; Kaufman, Albert; Calvert, Howard F
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1953
Added to NTRS: 2006-11-06
Accession Number: 93R17011; Document ID: 19930087721; Report Number: NACA-RM-E53C25
Investigation of the effect of impact damage on fatigue strength of jet-engine compressor rotor blades
Author(s): Kaufman, Albert; Meyer, Andre J , Jr
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1956
Added to NTRS: 2006-11-06
Accession Number: 93R13407; Document ID: 19930084117; Report Number: NACA-TN-3275
Investigation of mechanical fastenings for solid turbine blades made from ductile materials
Author(s): Meyer, Andre J , Jr; Kaufman, Albert; Caywood, W C
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1954
Added to NTRS: 2006-11-06
Accession Number: 93R18569; Document ID: 19930089279; Report Number: NACA-RM-E54E21
The design of brittle-material blade roots based on theory and rupture tests of plastic models
Author(s): Meyer, Andre J , Jr; Kaufman, Albert; Caywood, William C
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1956
Added to NTRS: 2006-11-06
Accession Number: 93R13766; Document ID: 19930084476; Report Number: NACA-TN-3773
Method for determining the need to rework or replace compressor rotor blades damaged by foreign objects
Author(s): Kaufman, Albert
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1958
Added to NTRS: 2006-11-06
Accession Number: 93R14421; Document ID: 19930085131; Report Number: NACA-TN-4324
Correlation of vibratory root failures and stress distribution in J65 compressor blades
Author(s): Meyer, Andre J , Jr; Kaufman, Albert
Abstract: No Abstract Available
NASA Center: Glenn Research Center Publication Year: 1955
Added to NTRS: 2006-11-06
Accession Number: 93R18089; Document ID: 19930088799; Report Number: NACA-RM-E54L24
Design of a high-temperature experiment for evaluating advanced structural materials
Author(s): Mockler, Theodore T.; Castro-Cedeno, Mario; Gladden, Herbert J.; Kaufman, Albert
Abstract: This report describes the design of an experiment for evaluating monolithic and composite material specimens in a high-temperature environment and subject to big thermal gradients. The material specimens will be exposed to ...
NASA Center: Glenn Research Center Publication Year: 1992
Added to NTRS: 2005-08-25
Accession Number: 93N11624; Document ID: 19930002436; Report Number: E-6287, NAS 1.15:105833, NASA-TM-105833
Thermal finite-element analysis of space shuttle main engine turbine blade
Author(s): Abdul-Aziz, Ali; Tong, Michael T.; Kaufman, Albert
Abstract: Finite-element, transient heat transfer analyses were performed for the first-stage blades of the space shuttle main engine (SSME) high-pressure fuel turbopump. The analyses were based on test engine data provided by ...
NASA Center: Glenn Research Center Publication Year: 1987
Added to NTRS: 2005-08-25
Accession Number: 88N13745; Document ID: 19880004363; Report Number: E-3535, NAS 1.15:100117, NASA-TM-100117
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