Turbulence in the Wake of a Thin Airfoil at Low Speeds Metadata

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Title

  • Main Title Turbulence in the Wake of a Thin Airfoil at Low Speeds
  • Series Title NACA Technical Memorandums

Creator

  • Author: Campbell, George S.
    Creator Type: Personal

Contributor

  • Originator: California Institute of Technology
    Contributor Type: Organization

Date

  • Creation: 1957-01

Language

  • English

Description

  • Content Description: From Summary: "Experiments have been made to determine the nature of turbulence in the wake of a two-dimensional airfoil at low speeds. The experiments were motivated by the need for data which can be used for analysis of the tail-buffeting problem in aircraft design. Turbulent intensity and power spectra of the velocity fluctuations were measured at a Reynolds number of 1.6 x 10(exp 5) for several angles of attack. Total-head measurements were also obtained in an attempt to relate steady and fluctuating wake properties."
  • Physical Description: 63 p.

Subject

  • Keyword: aerodynamics
  • Keyword: airfoils
  • Keyword: aircraft turbulence

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/2060/20040034247
  • Report No.: NACA-TM-1427
  • Center for AeroSpace Information Number: 20040034247
  • Archival Resource Key: ark:/67531/metadc64036