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

  • Author: Gray, V. H.
    Creator Type: Personal
  • Author: Bowden, D. T.
    Creator Type: Personal
  • Author: von Glahn, U.
    Creator Type: Personal

Contributor

  • Originator: Lewis Flight Propulsion Laboratory
    Contributor Type: Organization
    Contributor 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

  • Name: National Advisory Committee for Aeronautics Collection
    Code: NACA
  • Name: Technical Report Archive and Image Library
    Code: TRAIL

Institution

  • Name: UNT Libraries Government Documents Department
    Code: 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
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