Effects of leading-edge radius on the longitudinal stability characteristics of two 60 degree sweptback wings at high Reynolds numbers Metadata

Metadata describes a digital item, providing (if known) such information as creator, publisher, contents, size, relationship to other resources, and more. Metadata may also contain "preservation" components that help us to maintain the integrity of digital files over time.

Title

  • Main Title Effects of leading-edge radius on the longitudinal stability characteristics of two 60 degree sweptback wings at high Reynolds numbers
  • Series Title NACA Research Memorandums

Creator

  • Author: Schneider, William C.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1956-03-19

Language

  • English

Description

  • Content Description: Report presenting tests on two 60 degree sweptback wings of aspect ratios 2 and 3 to provide information on the influence of leading-edge radius on the static longitudinal stability characteristics of swept wings.
  • Physical Description: 46 p. : ill.

Subject

  • Keyword: aircraft stability
  • Keyword: sweptback wings

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: 93R18522
  • URL: http://hdl.handle.net/2060/19930089232
  • Report No.: NACA-RM-L55L30
  • Center for AeroSpace Information Number: 19930089232
  • Archival Resource Key: ark:/67531/metadc62443
Back to Top of Screen