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A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 3 Metadata

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Title

  • Main Title A flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 3
  • Series Title NACA Research Memorandums

Creator

  • Author: White, Maurice D.
    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: 1955-06-24

Language

  • English

Description

  • Content Description: Report presenting free-falling recoverable-model tests at transonic speeds on a model with a triangular wing of aspect ratio 3 and a 45 degree swept tail located in the chord plane of the wing. Static and dynamic longitudinal-stability data for the complete model, force and moment data for the major components of the model, and load distributions over the fuselage of the model were evaluated at a range of angles of attack. results regarding lift, drag, static longitudinal stability, dynamic longitudinal stability, horizontal-tail effectiveness, loading distributions over fuselage, and buffet boundary are provided.
  • Physical Description: 39 p. : ill.

Subject

  • Keyword: triangular wings
  • Keyword: aircraft stability
  • 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: 93R17956
  • URL: http://hdl.handle.net/2060/19930088666
  • Report No.: NACA-RM-A55D18
  • Center for AeroSpace Information Number: 19930088666
  • Archival Resource Key: ark:/67531/metadc61266
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