A Summary Report on the Effects of Mach Number on the Span Load Distribution on Wings of Several Models Metadata

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Title

  • Main Title A Summary Report on the Effects of Mach Number on the Span Load Distribution on Wings of Several Models
  • Series Title NACA Research Memorandums

Creator

  • Author: Jessen, Henry, Jr.
    Creator Type: Personal

Contributor

  • Originator: Ames Aeronautical Laboratory (U.S.)
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Ames Aeronautical Lab

Date

  • Creation: 1947-07-15

Language

  • English

Description

  • Content Description: Memorandum presenting an investigation of the change in spanwise load distribution at high Mach numbers, which is of considerable interest because lateral movement of the center of lift affects the trim, stability, and structural factors of safety of an airplane. The data is not sufficient to permit isolation of the effects of changes in wing configuration, but in a majority of cases, the tests reveal a tendency for the center of lift to shift outboard with increasing Mach number.
  • Physical Description: [21] p. : ill.

Subject

  • Keyword: aircraft wings
  • Keyword: load distributions

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: 93R14866
  • URL: http://hdl.handle.net/2060/19930085576
  • Report No.: NACA-RM-A7C28
  • Center for AeroSpace Information Number: 19930085576
  • Archival Resource Key: ark:/67531/metadc57986