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A DESIGN CALCULATION PROCEDURE FOR SHOCK-FREE OR STRONG PASSAGE SHOCK TURBOMACHINERY CASCADES
- Author
-
SIU SHING TONG; THOMPKINS WT JR
MASSACHUSETTS INST. TECHNOLOGY, DEP. AERONAUTICS ASTRONAUTICS/CAMBRIDGE MA 02139/USA - Source
- JOURNAL OF ENGINEERING FOR POWER; ISSN 0022-0825; USA; DA. 1983; VOL. 105; NO 2; PP. 369-376; BIBL. 10 REF.
- Document type
-
Article
- Language
- English
- Keyword (fr)
- CASCADE PROFIL ECOULEMENT SUPERSONIQUE METHODE CALCUL
- Keyword (en)
- AEROFOIL CASCADE SUPERSONIC FLOW CALCULATING METHOD
- Classification
-
- Pascal
- 001 Exact sciences and technology / 001B Physics
- Discipline
- Theoretical physics
- Origin
-
Inist-CNRS
- Database
- PASCAL
- INIST identifier
- PASCAL83X0392378
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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