Forces on elliptic cylinders in uniform air stream Metadata
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Title
- Main Title Forces on elliptic cylinders in uniform air stream
- Series Title NACA Technical Reports
Creator
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Author: Zahm, A. F.Creator Type: Personal
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Author: Smith, R. H.Creator Type: Personal
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Author: Louden, F. A.Creator Type: Personal
Contributor
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Originator: Bureau of Construction and Repair (Navy). Aerodynamical LaboratoryContributor Type: Organization
Date
- Creation: 1929
Language
- English
Description
- Content Description: From Summary: "This report presents the results of wind tunnel tests on four elliptic cylinders with various fineness ratios, conducted in the Navy Aerodynamic Laboratory, Washington. The object of the tests was to investigate the characteristics of sections suitable for streamline wire which normally has an elliptic section with a fineness ratio of 4.0; also to learn whether a reduction in fineness ratio would result in improvement; also to determine the pressure distribution on the model of fineness ratio of 4. Four elliptic cylinders with fineness ratios of 2.5, 3.0, 3.5, and 4.0 were made and then tested in the 8 by 8 wind tunnel; first, for cross-wind force, drag, and yawing moment at 30 miles an hour and various angles of yaw; next for drag 0 degree pitch and 0 degree yaw and various wind speeds; then for end effect on the smallest and largest models; and lastly for pressure distribution over the surface of the largest model at 0 degree pitch and 0 degree yaw and various wind speeds."
- Physical Description: 215 - 232 p. : ill.
Subject
- Keyword: fineness ratios
- Keyword: pressure distributions
- Keyword: aerodynamics
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: 93R20648
- URL: http://hdl.handle.net/2060/19930091358
- Report No.: NACA-TR-289
- Center for AeroSpace Information Number: 19930091358
- Archival Resource Key: ark:/67531/metadc65943