A graphical method of determining pressure distribution in two-dimensional flow Metadata
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Title
- Main Title A graphical method of determining pressure distribution in two-dimensional flow
- Series Title NACA Technical Reports
Creator
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Author: Jones, Robert T.Creator Type: Personal
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Author: Cohen, DorisCreator Type: Personal
Contributor
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Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
Date
- Creation: 1940-11-12
Language
- English
Description
- Content Description: By a generalization of the Joukowski method, a procedure is developed for effecting localized modifications of airfoil shapes and for determining graphically the resultant changes in the pressure distribution. The application of the procedure to the determination of the pressure distribution over airfoils of original design is demonstrated. Formulas for the lift, the moment, and the aerodynamic center are also given.
- Physical Description: 313 - 319 p. : ill.
Subject
- Keyword: flow characteristics
- Keyword: pressure distribution
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: 93R21090
- URL: http://hdl.handle.net/2060/19930091800
- Report No.: NACA-TR-722
- Center for AeroSpace Information Number: 19930091800
- Archival Resource Key: ark:/67531/metadc59971