Aerodynamic Characteristics of Four NACA Airfoil Sections Designed for Helicopter Rotor Blades Metadata
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Title
- Main Title Aerodynamic Characteristics of Four NACA Airfoil Sections Designed for Helicopter Rotor Blades
- Series Title NACA Wartime Reports
- Series Title NACA Restricted Bulletins
Creator
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Author: Stivers, Louis S., Jr.Creator Type: Personal
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Author: Rice, Fred J., Jr.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: 1946-02
Language
- English
Description
- Content Description: "The purpose of the present work is to extend the previous investigation and to derive additional airfoil sections designed to minimize the undesirable characteristics of the previously tested airfoils. The tests of these additional airfoils were made in the Langley two-dimensional low-turbulence tunnel (LTT)" (p. 2).
- Physical Description: 15 p. : ill.
Subject
- Keyword: airfoils
- Keyword: testing
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: 93R22071
- URL: http://hdl.handle.net/2060/19930092781
- Report No.: NACA-WR-L-29
- Report No.: NACA-RB-L5K02
- Center for AeroSpace Information Number: 19930092781
- Archival Resource Key: ark:/67531/metadc61378