3 edition of Application of a quasi-3D inviscid flow and boundary layer analysis to the hub-shroud contouring of a radial turbine found in the catalog.
Application of a quasi-3D inviscid flow and boundary layer analysis to the hub-shroud contouring of a radial turbine
Published
1984
by National Aeronautics and Space Administration in [Washington, D.C.?
.
Written in English
Edition Notes
Statement | Kestutis C. Civinskas and Louis A. Povinelli. |
Series | NASA technical memorandum -- 83669., USAAVSCOM technical report -- 84-C-1., AVSCOM technical report -- 84-C-1. |
Contributions | Povinelli, Louis A., United States. National Aeronautics and Space Administration. |
The Physical Object | |
---|---|
Format | Microform |
Pagination | 1 v. |
ID Numbers | |
Open Library | OL18040012M |
Taxation : convention between the Government of Canada and the Government of the Argentine Republic for the avoidance of double taxation and the prevention of fiscal evasion with respect to taxes on income and on capital (with protocol), Buenos Aires, April 29, 1993, in force December 30, 1994 with effect from January 1, 1995 =
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