Investigation of Extreme Leading-Edge Roughness on Thick Low-Drag Airfoils to Indicate Those Critical to Separation Metadata
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Title
- Main Title Investigation of Extreme Leading-Edge Roughness on Thick Low-Drag Airfoils to Indicate Those Critical to Separation
- Series Title NACA Wartime Reports
- Series Title NACA Confidential Bulletins
Creator
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Author: Davidson, MiltonCreator Type: Personal
Contributor
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Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
Date
- Creation: 1942-06
Language
- English
Description
- Content Description: Bulletin presenting a study of several airfoils, including a conventional NACA 23021 and some low-drag airfoils for which the thickness had been increased, as smooth airfoils and after the application of a standard roughness. The results show some of the airfoils to be critical to separation resulting from such flow disturbances.
- Physical Description: [15] p.
Subject
- Keyword: airfoils
- Keyword: leading-edge roughness
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: 93R22046
- URL: http://hdl.handle.net/2060/19930092756
- Report No.: NACA-WR-L-659
- Center for AeroSpace Information Number: 19930092756
- Report No.: NACA-CB
- Archival Resource Key: ark:/67531/metadc61332