Theoretical investigation of longitudinal response characteristics of a swept-wing fighter airplane having a normal acceleration control system and a comparison with other types of systems

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Description

Report presenting an investigation of the longitudinal response characteristics of a swept-wing fighter airplane using normal-acceleration control system. Results regarding the frequency and transient responses, acceleration systems, pitching-velocity command system, and the pitch-attitude system are provided.

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51 p. : ill.

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Stokes, Fred H. & Mathews, Charles W. July 1954.

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and one other and was provided by UNT Libraries Government Documents Department to Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 255 times . More information about this report can be viewed below.

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  • Main Title: Theoretical investigation of longitudinal response characteristics of a swept-wing fighter airplane having a normal acceleration control system and a comparison with other types of systems
  • Series Title: NACA Technical Notes

Description

Report presenting an investigation of the longitudinal response characteristics of a swept-wing fighter airplane using normal-acceleration control system. Results regarding the frequency and transient responses, acceleration systems, pitching-velocity command system, and the pitch-attitude system are provided.

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51 p. : ill.

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  • Accession or Local Control No: 93R13341
  • URL: http://hdl.handle.net/2060/19930084051 External Link
  • Report No.: NACA-TN-3191
  • Center for AeroSpace Information Number: 19930084051
  • Archival Resource Key: ark:/67531/metadc57313

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National Advisory Committee for Aeronautics Collection

The National Advisory Committee for Aeronautics (NACA) was a U.S. federal agency founded on March 3, 1915 to undertake, promote, and institutionalize aeronautical research. On October 1, 1958 the agency was dissolved, and its assets and personnel transferred to the newly created National Aeronautics and Space Administration (NASA).

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  • July 1954

Added to The UNT Digital Library

  • Nov. 16, 2011, 7:33 a.m.

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  • April 6, 2018, 1:58 p.m.

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Stokes, Fred H. & Mathews, Charles W. Theoretical investigation of longitudinal response characteristics of a swept-wing fighter airplane having a normal acceleration control system and a comparison with other types of systems, report, July 1954; (digital.library.unt.edu/ark:/67531/metadc57313/: accessed February 18, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.