The Landing Stability of a Powered Dynamic Model of a Flying Boat With a 30 Degree V-Step and With Two Depths of Transverse Step

One of 116 reports in the series: NACA Restricted Bulletins available on this site.

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Description

Report discusses tests conducted using a model of a four-engine long-range flying boat with a 30 degree V-step and two different transverse steps of comparable positions and depths. The limits of stability, landing speed, and landing characteristics of the different models are presented.

Physical Description

[7] p. : ill.

Creation Information

Parkinson, John B. & Land, Norman S. February 1944.

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided by the UNT Libraries Government Documents Department to the UNT Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 135 times. More information about this report can be viewed below.

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Description

Report discusses tests conducted using a model of a four-engine long-range flying boat with a 30 degree V-step and two different transverse steps of comparable positions and depths. The limits of stability, landing speed, and landing characteristics of the different models are presented.

Physical Description

[7] p. : ill.

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  • Accession or Local Control No: 93R21783
  • URL: http://hdl.handle.net/2060/19930092493 External Link
  • Report No.: NACA-WR-L-236
  • Report No.: NACA-RB-4B14
  • Center for AeroSpace Information Number: 19930092493
  • Archival Resource Key: ark:/67531/metadc60902

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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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Creation Date

  • February 1944

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • Jan. 14, 2019, 10:55 a.m.

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Parkinson, John B. & Land, Norman S. The Landing Stability of a Powered Dynamic Model of a Flying Boat With a 30 Degree V-Step and With Two Depths of Transverse Step, report, February 1944; (https://digital.library.unt.edu/ark:/67531/metadc60902/: accessed April 25, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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