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Effect of inducer inlet and diffuser throat areas on performance of a low pressure ratio sweptback centrifugal compressor

By: Hugh A. Klassen.
Material type: materialTypeLabelBookPublisher: Subject(s): Us National Aeronautics And Space AdministrationDDC classification: TR | TMX-3148
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Item type Current location Collection Call number Status Date due Barcode Item holds
Technical Report Technical Report PK Kelkar Library, IIT Kanpur
General Stacks TR TMX-3148 (Browse shelf) Not for loan TR2749
Total holds: 0

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