Analysis of Wind-Tunnel Tests to a Mach Number of 0.90 of a Four-Engine Propeller-Driven Airplane Configuration Having a Wing With 40 Degrees of Sweepback and an Aspect Ratio of 10 Metadata

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Title

  • Main Title Analysis of Wind-Tunnel Tests to a Mach Number of 0.90 of a Four-Engine Propeller-Driven Airplane Configuration Having a Wing With 40 Degrees of Sweepback and an Aspect Ratio of 10
  • Series Title NACA Technical Notes

Creator

  • Author: Edwards, George G.
    Creator Type: Personal
  • Author: Buell, Donald A.
    Creator Type: Personal
  • Author: Demele, Fred A.
    Creator Type: Personal
  • Author: Sutton, Fred B.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1956-09

Language

  • English

Description

  • Content Description: Report presenting an investigation at speeds of up to Mach number 0.90 to determine the effects of operating propellers on the longitudinal characteristics of a four-engine tractor airplane configuration with a 40 degree swept wing with an aspect ratio of 10. Results regarding low-speed conditions, high-speed conditions, components of lift, effect of configuration changes, longitudinal stability, and the reduction of adverse effects of propellers on stability are provided.
  • Physical Description: 170 p. : ill.

Subject

  • Keyword: aircraft propellers
  • Keyword: aircraft stability
  • Keyword: longitudinal 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: 93R13788
  • URL: http://hdl.handle.net/2060/19930084498
  • Report No.: NACA-TN-3790
  • Center for AeroSpace Information Number: 19930084498
  • Archival Resource Key: ark:/67531/metadc56014