Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing Metadata
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Title
- Main Title Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing
- Series Title NACA Research Memorandums
Creator
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Author: Hanson, Perry W.Creator Type: Personal
Contributor
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Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: NASA Langley Research Center
Date
- Creation: 1957-10-16
Language
- English
Description
- Content Description: Report presenting an investigation to determine the effects of simulated engine nacelles and wing-root freedoms on the flutter characteristics of a cambered, modified, swept, tapered, semispan wing through a range of Mach numbers. Wings were tested with and without nacelles and with the model restrained, free to roll, and free to translate in the vertical direction. Results regarding the effect of nacelles, flutter boundary, and effect of wing-mount freedom are provided.
- Physical Description: 44 p. : ill.
Subject
- Keyword: aircraft wings
- Keyword: nacelles
- Keyword: aircraft stability
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: 71N70514
- URL: http://hdl.handle.net/2060/19710065201
- Report No.: NACA-RM-L57H16
- Center for AeroSpace Information Number: 19710065201
- Archival Resource Key: ark:/67531/metadc53182