Investigation of interference lift, drag, and pitching moment of a series of triangular-wing and body combinations at a Mach number of 1.94 Metadata

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Title

  • Main Title Investigation of interference lift, drag, and pitching moment of a series of triangular-wing and body combinations at a Mach number of 1.94
  • Series Title NACA Research Memorandums

Creator

  • Author: Coletti, Donald E.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1955-12-21

Language

  • English

Description

  • Content Description: Report presenting an investigation at Mach number 1.94 of a series of triangular-wing and body combinations to determine the interference lift, drag, and pitching moment. The models had a series of seven flat-plate triangular wings of varying scale, four with semiapex angles of 30 degrees, and three with semiapex angles of 45 degrees. Results indicated that the interference between the wing and the body gave an increase in lift over the wing and body alone, but at the expense of more drag.

Subject

  • Keyword: aircraft design
  • Keyword: aircraft wings
  • 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: 93R18186
  • URL: http://hdl.handle.net/2060/19930088896
  • Report No.: NACA-RM-L55I14
  • Center for AeroSpace Information Number: 19930088896
  • Archival Resource Key: ark:/67531/metadc61653