Critical Mach Numbers of Thin Airfoil Sections with Plain Flaps Metadata

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Title

  • Main Title Critical Mach Numbers of Thin Airfoil Sections with Plain Flaps
  • Series Title NACA Wartime Reports
  • Series Title NACA Advanced Confidential Reports

Creator

  • Author: Pardee, Otway O'M.
    Creator Type: Personal
  • Author: Heaslet, Max A.
    Creator Type: Personal

Contributor

  • Originator: Ames Aeronautical Laboratory (U.S.)
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Ames Aeronautical Lab
  • Originator: United States. National Advisory Committee for Aeronautics.
    Contributor Type: Organization

Date

  • Creation: 1946-04

Language

  • English

Description

  • Content Description: Critical Mach number as function of lift coefficient is determined for certain moderately thick NACA low-drag airfoils. Results, given graphically, included calculations on same airfoil sections with plain flaps for small flap deflections. Curves indicate optimum critical conditions for airfoils with flaps in such form that they can be compared with corresponding results for zero flap deflections. Plain flaps increase life-coefficient range for which critical Mach number is in region of high values characteristic of low-drag airfoils.
  • Physical Description: [25] p.

Subject

  • Keyword: airfoils
  • Keyword: aircraft flaps

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: 93R22024
  • URL: http://hdl.handle.net/2060/19930092734
  • Report No.: NACA-WR-W-2
  • Report No.: NACA-ACR-6A30
  • Center for AeroSpace Information Number: 19930092734
  • Archival Resource Key: ark:/67531/metadc61295
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