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Design Evaluation Using Finite Element Analysis of Cooled Silicon Nitride Plates for a Turbine Blade Application [microform]

Ali Abdul-Aziz, George Y. Baaklini, Ramakrishna T. Bhatt
Format
EBook; Book; Government Document; Microform; Online
Published
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
Language
English
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:210819
Description
1 v.
Notes
Shipping list no.: 2002-0336-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 1 microfiche.
Series Statement
[NASA technical memorandum] ; NASA/TM-2001-210819
NASA technical memorandum 210819
Other Forms
Also available via Internet from the NASA web site. Address as of 10/17/02: http://gltrs.grc.nasa.gov/reports/2001/TM-2001-210 819.pdf ; current access is available via PURL.
Copyright Not EvaluatedCopyright Not Evaluated
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| 2
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    a| Silicon nitrides. 2| nasat
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    7
    a| Finite element method. 2| nasat
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    a| Thermal stresses. 2| nasat
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    7
    a| Thermal environments. 2| nasat
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    7
    a| Hole geometry (Mechanics). 2| nasat
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    7
    a| Air cooling. 2| nasat
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    7
    a| Thermodynamic efficiency. 2| nasat
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    a| Ceramics. 2| nasat
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    7
    a| Temperature distribution. 2| nasat
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    7
    a| Stress analysis. 2| nasat
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    7
    a| Ceramic coatings. 2| nasat
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    a| Baaklini, George Y.
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