Low-lift drag and stability data from rocket models of a modified-delta-wing airplane with and without external stores at Mach numbers from 0.8 to 1.36 Metadata

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Title

  • Main Title Low-lift drag and stability data from rocket models of a modified-delta-wing airplane with and without external stores at Mach numbers from 0.8 to 1.36
  • Series Title NACA Research Memorandums

Creator

  • Author: Mitcham, Grady L.
    Creator Type: Personal
  • Author: Blanchard, Willard S., Jr.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1953-03-26

Language

  • English

Description

  • Content Description: Report presenting a flight investigation to determine the drag and stability at low lift coefficients of models of a modified-delta-wing airplane at a range of Mach and Reynolds numbers. A summary of the drag and stability data from the tests is provided.
  • Physical Description: 43 p. : ill.

Subject

  • Keyword: drag characteristics
  • Keyword: aircraft stability

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: 93R16809
  • URL: http://hdl.handle.net/2060/19930087519
  • Report No.: NACA-RM-L53A27
  • Center for AeroSpace Information Number: 19930087519
  • Archival Resource Key: ark:/67531/metadc59563