Wind-tunnel investigation at Mach numbers from 0.50 to 1.29 of an unswept tapered wing of aspect ratio 2.67 with leading- and trailing-edge flaps - trailing-edge flaps deflected Metadata
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Title
- Main Title Wind-tunnel investigation at Mach numbers from 0.50 to 1.29 of an unswept tapered wing of aspect ratio 2.67 with leading- and trailing-edge flaps - trailing-edge flaps deflected
- Series Title NACA Research Memorandums
Creator
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Author: Stivers, Louis S., Jr.Creator Type: Personal
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Author: Malick, Alexander W.Creator Type: Personal
Contributor
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Originator: Ames Aeronautical Laboratory (U.S.)Contributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Ames Aeronautical Lab
Date
- Creation: 1950-12-13
Language
- English
Description
- Content Description: Report presenting aerodynamic characteristics of an unswept wing with an aspect ratio of 2.67, a taper ratio of 0.5, and employing full-span, 25-percent chord, plain, trailing-edge flaps using wind-tunnel testing of a semispan model. The trailing-edge flap was generally effective in changing the lift coefficient at each angle of attack and Mach number of the investigation. Results regarding lift characteristics, hinge-moment characteristics, drag characteristics, and pitching-moment characteristics are provided.
- Physical Description: 45 p. : ill.
Subject
- Keyword: aerodynamics
- Keyword: aircraft flaps
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: 93R15685
- URL: http://hdl.handle.net/2060/19930086395
- Report No.: NACA-RM-A50J09b
- Center for AeroSpace Information Number: 19930086395
- Archival Resource Key: ark:/67531/metadc58635