Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades Metadata

Metadata describes a digital item, providing (if known) such information as creator, publisher, contents, size, relationship to other resources, and more. Metadata may also contain "preservation" components that help us to maintain the integrity of digital files over time.

Title

  • Main Title Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades
  • Series Title NACA Wartime Reports
  • Series Title NACA Restricted Bulletins

Creator

  • Author: Rice, Fred J , Jr
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1946-02

Language

  • English

Description

  • Content Description: From Introduction: "The purpose of the present work is to extend the previous investigation and to derive additional airfoil sections designed to minimize the undesirable characteristics of the previously tested airfoils. The tests of these additional airfoils were made in the Langley two-dimensional low-turbulence tunnel (LTT)."
  • Physical Description: 15 p. : ill.

Subject

  • Keyword: airfoils
  • Keyword: testing

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

  • 93R22071
  • URL: http://hdl.handle.net/2060/19930092781
  • Report No.: NACA-WR-L-29
  • Report No.: NACA-RB-L5K02
  • Center for AeroSpace Information Number: 19930092781
  • Archival Resource Key: ark:/67531/metadc61378