A low-speed investigation of the aerodynamic, control, and hinge-moment characteristics of two types of controls and balancing tabs on a large-scale thin delta-wing-fuselage model

One of 5,163 reports in the series: NACA Research Memorandums available on this site.

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Description

Report presenting a low-speed investigation of the aerodynamic and control characteristics of a 3-percent-thick, 60 degree delta-wing-fuselage configuration in the full-scale tunnel to obtain data at large scale on control configurations of general interest and to determine whether significant Reynolds number effects existed for a very thin wing subject to leading-edge vortex-type flow. Aerodynamic forces, moments, and hinge moments were obtained for several types of controls and flap deflections.

Physical Description

69 p. : ill.

Creation Information

Fink, Marvin P. & Cocke, Bennie W. March 24, 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 25 times . More information about this report can be viewed below.

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  • Main Title: A low-speed investigation of the aerodynamic, control, and hinge-moment characteristics of two types of controls and balancing tabs on a large-scale thin delta-wing-fuselage model
  • Series Title: NACA Research Memorandums

Description

Report presenting a low-speed investigation of the aerodynamic and control characteristics of a 3-percent-thick, 60 degree delta-wing-fuselage configuration in the full-scale tunnel to obtain data at large scale on control configurations of general interest and to determine whether significant Reynolds number effects existed for a very thin wing subject to leading-edge vortex-type flow. Aerodynamic forces, moments, and hinge moments were obtained for several types of controls and flap deflections.

Physical Description

69 p. : ill.

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Identifier

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  • Accession or Local Control No: 93R17518
  • URL: http://hdl.handle.net/2060/19930088228 External Link
  • Report No.: NACA-RM-L54B03
  • Center for AeroSpace Information Number: 19930088228
  • Archival Resource Key: ark:/67531/metadc60454

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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).

Technical Report Archive and Image Library

This selection of materials from the Technical Report Archive and Image Library (TRAIL) includes hard-to-find reports published by various government agencies. The technical publications contain reports, images, and technical descriptions of research performed for U.S. government agencies. Topics range from mining, desalination, and radiation to broader physics, biology, and chemistry studies. Some reports include maps, foldouts, blueprints, and other oversize materials.

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Creation Date

  • March 24, 1954

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • April 2, 2018, 7:13 p.m.

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Citations, Rights, Re-Use

Fink, Marvin P. & Cocke, Bennie W. A low-speed investigation of the aerodynamic, control, and hinge-moment characteristics of two types of controls and balancing tabs on a large-scale thin delta-wing-fuselage model, report, March 24, 1954; (digital.library.unt.edu/ark:/67531/metadc60454/: accessed April 25, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.