AN ANALYTICAL STUDY OF THE EFFECTS OF TURBINE VARIABLE GEOMETRY OPERATION ON TURBINE BLADE COOLING REQUIREMENTS FOR FIXED MATCH POINT TURBOJET APPLICATION.
- Author
- NEALY DA; LUEDERS HG
GENERAL MOTORS CORP. - Source
- S.A.E. TRANS.; U.S.A.; DA. 1976 PARU 1977; VOL. 85; PART. 4; PP. 2864-2879; BIBL. 2 REF.
- Document type
- Article
- Language
- English
- Keyword (fr)
- PROPULSEUR REACTION TURBINE GAZ TURBOREACTEUR AUBE REFROIDISSEMENT ECOULEMENT GEOMETRIE VARIABLE CONCEPTION TEMPERATURE INDUSTRIE MECANIQUE
- Keyword (en)
- PROPELLER JET ENGINE GAS TURBINE TURBOJET AUBE COOLING FLOW VARIABLE GEOMETRY DESIGN TEMPERATURE MECHANICAL ENGINEERING
- Keyword (es)
- INDUSTRIA MECANICA
- Classification
- Discipline
- Building. Public works. Transport. Civil engineering
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- PASCAL7880325062
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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