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The Effect of Mach Number on the Aerodynamic Characteristics of a Single-Engine Pursuit Airplane as Determined From Tests of a 1/3-Scale Model Metadata

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Title

  • Main Title The Effect of Mach Number on the Aerodynamic Characteristics of a Single-Engine Pursuit Airplane as Determined From Tests of a 1/3-Scale Model
  • Series Title NACA Wartime Reports
  • Series Title NACA Memorandum Reports

Creator

  • Author: Robinson, Robert C.
    Creator Type: Personal
  • Author: Jessen, Henry
    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: 1945-05-03

Language

  • English

Description

  • Content Description: Report discussing the effects of Mach number on the aerodynamic characteristics of an Allison powered single-engine pursuit airplane. Information about the lift, drag, pitching-moment characteristics, stability, tail effectiveness, and elevator effectiveness with Mach number is provided.
  • Physical Description: [29] p. : ill.

Subject

  • Keyword: Allison airplane
  • Keyword: aerodynamics
  • Keyword: aircraft performance

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: 93R21983
  • URL: http://hdl.handle.net/2060/19930092693
  • Report No.: NACA-WR-A-76
  • Report No.: NACA-MR-A5E03
  • Center for AeroSpace Information Number: 19930092693
  • Archival Resource Key: ark:/67531/metadc61229
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