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Title: Rotational Compressible Inverse Design Method for Two-Dimensional Internal Flow Configurations
Keywords: Convergent divergent nozzle
Design;Inverse problem
Internal flow
Geometrical shape;Non viscous fluid
Compressible fluid;Pipe bend
Velocity distribution
Issue Date: 1993
Publisher: American Institute of Aeronautics and Astronautics
Citation: Αmerican Institute of Aeronautics & Αstronautics Journal, Vol. 31, no. 3 pp. 551-558
ISSN: 0001-1452
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Appears in Collections:Δημοσιεύσεις σε Περιοδικά

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