Aerodynamic performance of a ceramic-coated core turbine vane tested with cold air in a two-dimensional cascade

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049 ⊔ ⊔ ‡aUIUU
050 ⊔ 4 ‡aTL521.3.T4 ‡bA3 no. 3191
086 0 ⊔ ‡aNAS 1.15:X-3191
100 1 ⊔ ‡aStabe, Roy G.
245 1 0 ‡aAerodynamic performance of a ceramic-coated core turbine vane tested with cold air in a two-dimensional cascade / ‡cRoy G. Stabe and Curt H. Liebert.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1975.
300 ⊔ ⊔ ‡a13 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNASA technical memorandum ; ‡vNASA TM X-3191
500 ⊔ ⊔ ‡aPrepared at Lewis Research Center.
500 ⊔ ⊔ ‡aCover title.
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 8).
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aCeramic coating.
650 ⊔ 0 ‡aCascades (Fluid dynamics)
650 ⊔ 0 ‡aTurbines ‡xAerodynamics.
650 ⊔ 0 ‡aAircraft gas-turbines ‡xBlades ‡xCooling.
700 1 ⊔ ‡aLiebert, Curt H.
710 2 ⊔ ‡aLewis Research Center.
CID ⊔ ⊔ ‡a011426583
DAT 0 ⊔ ‡a20101008103525.0 ‡b20141013010000.0
DAT 1 ⊔ ‡a20141112173021.0 ‡b2023-03-14T18:16:22Z
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