Preliminary Results of Cyclical De-Icing of a Gas-Heated Airfoil Metadata
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Title
- Main Title Preliminary Results of Cyclical De-Icing of a Gas-Heated Airfoil
- Series Title NACA Research Memorandums
Creator
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Author: Gray, V. H.Creator Type: Personal
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Author: Bowden, D. T.Creator Type: Personal
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Author: von Glahn, U.Creator Type: Personal
Contributor
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Originator: Lewis Flight Propulsion LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab
Date
- Creation: 1952-01-24
Language
- English
Description
- Content Description: "An NACA 65(sub 1)-212 airfoil of 8-foot chord was provided with a gas-heated leading edge for investigations of cyclical de-icing. De-icing was accomplished with intermittent heating of airfoil segments that supplied hot gas to chordwise passages in a double-skin construction. Ice removal was facilitated by a spanwise leading-edge parting strip which was continuously heated from the gas-supply duct. Preliminary results demonstrate that satisfactory cyclical ice removal occurs with ratios of cycle time to heat-on period (cycle ratio) from 10 to 26" (p. 1).
- Physical Description: 38 p. : ill.
Subject
- Keyword: fluid mechanics and heat transfer
- Keyword: aircraft deicing
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: 81N73132
- URL: http://hdl.handle.net/2060/19810068710
- Report No.: NACA-RM-E51J29
- Center for AeroSpace Information Number: 19810068710
- Archival Resource Key: ark:/67531/metadc53515