Effects of leading-edge radius on the longitudinal stability characteristics of two 60 degree sweptback wings at high Reynolds numbers Metadata
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Title
- Main Title Effects of leading-edge radius on the longitudinal stability characteristics of two 60 degree sweptback wings at high Reynolds numbers
- Series Title NACA Research Memorandums
Creator
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Author: Schneider, William C.Creator Type: Personal
Contributor
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Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
Date
- Creation: 1956-03-19
Language
- English
Description
- Content Description: Report presenting tests on two 60 degree sweptback wings of aspect ratios 2 and 3 to provide information on the influence of leading-edge radius on the static longitudinal stability characteristics of swept wings.
- Physical Description: 46 p. : ill.
Subject
- Keyword: aircraft stability
- Keyword: sweptback wings
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: 93R18522
- URL: http://hdl.handle.net/2060/19930089232
- Report No.: NACA-RM-L55L30
- Center for AeroSpace Information Number: 19930089232
- Archival Resource Key: ark:/67531/metadc62443