Preliminary Results of an Investigation by the Wing-Flow Method of the Longitudinal Stability Characteristics of a 1/50-Scale Semispan Model of the McDonnell XP-88 Airplane Metadata

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Title

  • Main Title Preliminary Results of an Investigation by the Wing-Flow Method of the Longitudinal Stability Characteristics of a 1/50-Scale Semispan Model of the McDonnell XP-88 Airplane
  • Series Title NACA Research Memorandums

Creator

  • Author: Crane, Harold L.
    Creator Type: Personal

Contributor

  • Originator: Langley Aeronautical Laboratory
    Contributor Type: Organization
    Contributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
  • Originator: United States. Air Force. Air MateriĆ©l Command.
    Contributor Type: Organization

Date

  • Creation: 1948-06-09

Language

  • English

Description

  • Content Description: "This paper presents the results of measurements of longitudinal stability of a 1/50-scale model of the XP-88 airplane by the wing-flow method. Lift, rolling-moment, hinge-moment, and pitching-moment characteristics as well as the downwash at the tail were measured over a Mach number range from approximately 0.5 to 1.05 at Reynolds numbers below 1,000,000. No measurements of drag were obtained" (p. 1).
  • Physical Description: [27] p. : ill.

Subject

  • Keyword: wing-flow method
  • Keyword: aircraft stability
  • Keyword: McDonnell XP-88

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/2060/20050028619
  • Report No.: NACA-RM-SL8E28A
  • Center for AeroSpace Information Number: 20050028619
  • Archival Resource Key: ark:/67531/metadc64616
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