Effect of Increase in Angle of Dead Rise on the Hydrodynamic Qualities of a Seaplane Configuration Incorporating High Wing Loading Metadata

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Title

  • Main Title Effect of Increase in Angle of Dead Rise on the Hydrodynamic Qualities of a Seaplane Configuration Incorporating High Wing Loading
  • Series Title NACA Research Memorandums

Creator

  • Author: Kapryan, Walter J.
    Creator Type: Personal
  • Author: Weinstein, Irving
    Creator Type: Personal

Contributor

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

Date

  • Creation: 1956-10-31

Language

  • English

Description

  • Content Description: Memorandum presenting an investigation to determine the effects of increase in angle of dead rise on the overall hydrodynamic characteristics of a seaplane having a length-beam ratio of 15 and a wing loading of 120 pounds per square foot. In general, increasing the angle of dead rise from 20 to 40 degrees and 60 degrees improved the trim limits of stability and the range of center-of-gravity positions for satisfactory take-off characteristics.
  • Physical Description: 31 p. : ill.

Subject

  • Keyword: hydrodynamics
  • Keyword: seaplanes

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: 93R18785
  • URL: http://hdl.handle.net/2060/19930089495
  • Report No.: NACA-RM-L56H21
  • Center for AeroSpace Information Number: 19930089495
  • Archival Resource Key: ark:/67531/metadc62936