Gas turbine ceramic-coated-vane concept with convection-cooled porous metal core /

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Bibliographic Details
Corporate Authors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Lewis Research Center, Propulsion Laboratory (U.S.)
Other Authors: Kascak, Albert F.
Format: Government Document Book
Language:English
Published: Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981.
Series:NASA technical paper 1942.
AVRADCOM technical report ; 81-C-7.
Subjects:

MARC

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245 0 0 |a Gas turbine ceramic-coated-vane concept with convection-cooled porous metal core /  |c Albert F. Kascak [and others]. 
260 |a Washington, D.C. :  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch ;  |a [Springfield, Va.] :  |b [For sale by the National Technical Information Service],  |c 1981. 
300 |a 11 pages :  |b illustrations ;  |c 27 cm. 
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490 1 |a NASA technical paper;  |v 1942 
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500 |a "AVRADCOM Research and Technology Laboratories." 
500 |a "Lewis Research Center." 
500 |a "December 1981"--Cover. 
500 |a STAR Category 07. 
504 |a Includes bibliographical references. 
650 0 |a Aircraft gas-turbines  |x Blades  |x Testing. 
650 0 |a Thermal stresses. 
700 1 |a Kascak, Albert F. 
710 1 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch. 
710 2 |a Lewis Research Center. 
710 2 |a Propulsion Laboratory (U.S.) 
830 0 |a NASA technical paper  |v 1942. 
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