Expressions for Measuring the Accuracy of Approximate Solutions to Compressible Flow Through Cascades of Blades With Examples of Use Metadata
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Title
- Main Title Expressions for Measuring the Accuracy of Approximate Solutions to Compressible Flow Through Cascades of Blades With Examples of Use
- Series Title NACA Technical Notes
Creator
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Author: Sinnette, John T., Jr.Creator Type: Personal
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Author: Costello, George R.Creator Type: Personal
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Author: Cummings, Robert L.Creator Type: Personal
Contributor
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Originator: Lewis Flight Propulsion LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab
Date
- Creation: 1951-10
Language
- English
Description
- Content Description: Report presenting four necessary conditions for steady irrotational compressible flow through a straight cascade of blades as derived from the irrotationality condition and conservation of mass and momentum. The expressions used can only give an approximate solution to the conditions, as there are an infinite number of them.
- Physical Description: 33 p. : ill.
Subject
- Keyword: aerodynamics
- Keyword: flow compressibility
Collection
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Name: National Advisory Committee for Aeronautics CollectionCode: NACA
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Name: Technical Report Archive and Image LibraryCode: TRAIL
Institution
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Name: UNT Libraries Government Documents DepartmentCode: UNTGD
Rights
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
Resource Type
- Report
Format
- Text
Identifier
- Accession or Local Control No: 93R12710
- URL: http://hdl.handle.net/2060/19930083420
- Report No.: NACA-TN-2501
- Center for AeroSpace Information Number: 19930083420
- Archival Resource Key: ark:/67531/metadc56232