The relation between spanwise variations in the critical Mach number and spanwise load distributions Metadata

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Title

  • Main Title The relation between spanwise variations in the critical Mach number and spanwise load distributions
  • Series Title NACA Wartime Reports

Creator

  • Author: Whitcomb, Richard T.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1944-12

Language

  • English

Description

  • Content Description: "Data are presented to show the changes that occur in the spanwise load distributions on wings when the critical Mach number is exceeded. The data indicate that the magnitude of the changes in spanwise load distribution varies with the magnitude of the spanwise variation in the critical Mach numbers of the sections. Means of reducing the magnitudes of such changes are considered" (p. 1).
  • Physical Description: [9] p. : ill.

Subject

  • Keyword: aerodynamics
  • 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: 93R22012
  • URL: http://hdl.handle.net/2060/19930092722
  • Report No.: NACA-WR-L-182
  • Report No.: NACA-CB-L4L07
  • Center for AeroSpace Information Number: 19930092722
  • Archival Resource Key: ark:/67531/metadc61275