Free-flight investigation at transonic speeds of the power-on characteristics including some effects of sonic propulsive jets of a four-engine delta-wing configuration Metadata

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Title

  • Main Title Free-flight investigation at transonic speeds of the power-on characteristics including some effects of sonic propulsive jets of a four-engine delta-wing configuration
  • Series Title NACA Research Memorandums

Creator

  • Author: Judd, Joseph H.
    Creator Type: Personal
  • Author: Falanga, Ralph A.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1957-08-16

Language

  • English

Description

  • Content Description: Report presenting an investigation of a free-flight model of a delta-wing configuration with four engines mounted two to a nacelle below the wing with rocket turbojet simulators operating at a range of Mach numbers. Results regarding wing pressure coefficients, fuselage pressure coefficient, airplane aerodynamic characteristics, and airplane trim are provided.
  • Physical Description: 47 p. : ill.

Subject

  • Keyword: propulsive jet effects
  • Keyword: aerodynamics

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: 93R19020
  • URL: http://hdl.handle.net/2060/19930089730
  • Report No.: NACA-RM-L57E31
  • Center for AeroSpace Information Number: 19930089730
  • Archival Resource Key: ark:/67531/metadc63486