Comparison Between Theoretical and Experimental Rates of Roll of Two Models with Flexible Rectangular Wings at Supersonic Speeds Metadata

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Title

  • Main Title Comparison Between Theoretical and Experimental Rates of Roll of Two Models with Flexible Rectangular Wings at Supersonic Speeds
  • Series Title NACA Research Memorandums

Creator

  • Author: Hedgepeth, John M.
    Creator Type: Personal
  • Author: Kell, Robert J.
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1954-08-05

Language

  • English

Description

  • Content Description: "A comparison is presented between the experimentally measured and theoretically calculated (by the method of NACA TN 3067) rates of roll of two rocket-propelled models with flexible rectangular wings. The comparisons show that although there are large aeroelastic losses in rolling rate, the theory predicts the actual rate of roll accurately" (p. 1).
  • Physical Description: 21 p. : ill.

Subject

  • Keyword: flexible rectangular wings
  • Keyword: aircraft wings

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: 93R17606
  • URL: http://hdl.handle.net/2060/19930088316
  • Report No.: NACA-RM-L54F23
  • Center for AeroSpace Information Number: 19930088316
  • Archival Resource Key: ark:/67531/metadc60634
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