Wind-Tunnel Investigations on a Changed Mustang Profile with Nose Flap Force and Pressure-Distribution Measurements Metadata

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Title

  • Main Title Wind-Tunnel Investigations on a Changed Mustang Profile with Nose Flap Force and Pressure-Distribution Measurements
  • Series Title NACA Technical Memorandums
  • Parallel Title Windkanaluntersuchungen an einem abgeänderten Mustang-Profil mit Nasenklappe

Creator

  • Author: Krüger, W.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1947-09

Language

  • English

Description

  • Content Description: "Measurements are described which were taken in the large wind tunnel of the AVA on a rectangular wing "Mustang 2" with nose flap of a chord of 10 percent. Besides force measurements the results of pressure-distribution measurements are given and compared with those on the same profile "without" nose flap" (p. 1).
  • Physical Description: 18 p. : ill.

Subject

  • Keyword: wind tunnel testing
  • Keyword: aircraft wings
  • Keyword: nose flaps

Source

  • Untersuchungen und Mitteilungen; No. 3153

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/2060/20050031128
  • Report No.: NACA-TM-1177
  • Center for AeroSpace Information Number: 20050031128
  • Archival Resource Key: ark:/67531/metadc64848
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