Effects of independent variations of mach number and reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections Metadata

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Title

  • Main Title Effects of independent variations of mach number and reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections
  • Series Title NACA Technical Notes

Creator

  • Author: Racisz, Stanley F.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1952-11

Language

  • English

Description

  • Content Description: Report presenting an investigation in the low-turbulence pressure tunnel to determine the effects of Mach and Reynolds number on the maximum lift characteristics of the NACA 65-006, 64-009, 64-210, and 64(sub 2)-215 airfoil sections in smooth and leading-edge roughness conditions. A range of Mach and Reynolds numbers were explored.
  • Physical Description: [33] p. : ill.

Subject

  • Keyword: airfoils
  • Keyword: lift characteristics

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: 93R12763
  • URL: http://hdl.handle.net/2060/19930083473
  • Report No.: NACA-TN-2824
  • Center for AeroSpace Information Number: 19930083473
  • Archival Resource Key: ark:/67531/metadc56326