An engineering method for the determination of aeroelastic effects upon the rolling effectiveness of ailerons on swept wings Metadata

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Title

  • Main Title An engineering method for the determination of aeroelastic effects upon the rolling effectiveness of ailerons on swept wings
  • Series Title NACA Research Memorandums

Creator

  • Author: Strass, H. Kurt
    Creator Type: Personal
  • Author: Stephens, Emily W.
    Creator Type: Personal

Contributor

  • Originator: Langley Aeronautical Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab

Date

  • Creation: 1953-11-30

Language

  • English

Description

  • Content Description: Report presenting a method for calculating the steady-state rolling effectiveness of flexible sweptback wings at subsonic and supersonic speeds. Comparisons between the experimental and calculated values are presented for a wide range of wing-aileron configurations.
  • Physical Description: 82 p. : ill.

Subject

  • Keyword: rolling effectiveness
  • Keyword: wing-aileron configurations

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: 93R17079
  • URL: http://hdl.handle.net/2060/19930087789
  • Report No.: NACA-RM-L53H14
  • Center for AeroSpace Information Number: 19930087789
  • Archival Resource Key: ark:/67531/metadc59770