High-Speed Measurements on a Swept-Back Wing (Sweepback Angle phi = 35 Deg) Metadata

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Title

  • Main Title High-Speed Measurements on a Swept-Back Wing (Sweepback Angle phi = 35 Deg)
  • Series Title NACA Technical Memorandums

Creator

  • Author: Göthert, B.
    Creator Type: Personal

Contributor

  • Originator: United States. National Advisory Committee for Aeronautics.
    Contributor Type: Organization

Date

  • Creation: 1947-03

Language

  • English

Description

  • Content Description: "In the following, high-speed measurements on a swept-back wing are reported. The curves of lift, moment, and drag have been determined up to Mach numbers of M = 0.87, and they are compared to a rectangular wing. Through measurements of the total-head loss behind the wing and through schlieren pictures, an insight into the formation of the compression shock at high Mach numbers has been obtained" (p. 1).
  • Physical Description: [33] p. : ill.

Subject

  • Keyword: sweptback wings
  • Keyword: aerodynamics

Source

  • Lilienthal-Gesellschaft fuer Luftfahrtforschung; 30-40; Rept-156

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

  • URL: http://hdl.handle.net/2060/20050019388
  • Report No.: NACA-TM-1102
  • Center for AeroSpace Information Number: 20050019388
  • Archival Resource Key: ark:/67531/metadc64276