Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing Metadata

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Title

  • Main Title Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing
  • Series Title NACA Research Memorandums

Creator

  • Author: Hanson, Perry W.
    Creator Type: Personal

Contributor

  • Originator: Langley Aeronautical Laboratory
    Contributor Type: Organization
    Contributor Info: NASA Langley Research Center

Date

  • Creation: 1957-10-16

Language

  • English

Description

  • Content Description: Report presenting an investigation to determine the effects of simulated engine nacelles and wing-root freedoms on the flutter characteristics of a cambered, modified, swept, tapered, semispan wing through a range of Mach numbers. Wings were tested with and without nacelles and with the model restrained, free to roll, and free to translate in the vertical direction. Results regarding the effect of nacelles, flutter boundary, and effect of wing-mount freedom are provided.
  • Physical Description: 44 p. : ill.

Subject

  • Keyword: aircraft wings
  • Keyword: nacelles
  • Keyword: aircraft stability

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: 71N70514
  • URL: http://hdl.handle.net/2060/19710065201
  • Report No.: NACA-RM-L57H16
  • Center for AeroSpace Information Number: 19710065201
  • Archival Resource Key: ark:/67531/metadc53182
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