Investigation of the effect of spanwise positioning of a vertically symmetric ogive-cylinder nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6 with and without a fuselage

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Description

Report presenting an investigation of an ogive-cylinder nacelle in various spanwise locations in a vertically symmetric position on a small-size 45 degree sweptback wing of aspect ratio 6 with and without a fuselage. Results regarding the drag characteristics, lift-drag ratios, lift characteristics, pitch characteristics, and lateral center of pressure are provided.

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Silvers, H. Norman & King, Thomas J., Jr. October 7, 1953.

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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 302 times . More information about this report can be viewed below.

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  • Main Title: Investigation of the effect of spanwise positioning of a vertically symmetric ogive-cylinder nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6 with and without a fuselage
  • Series Title: NACA Research Memorandums

Description

Report presenting an investigation of an ogive-cylinder nacelle in various spanwise locations in a vertically symmetric position on a small-size 45 degree sweptback wing of aspect ratio 6 with and without a fuselage. Results regarding the drag characteristics, lift-drag ratios, lift characteristics, pitch characteristics, and lateral center of pressure are provided.

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  • Accession or Local Control No: 93R17049
  • URL: http://hdl.handle.net/2060/19930087759 External Link
  • Report No.: NACA-RM-L53H17
  • Center for AeroSpace Information Number: 19930087759
  • Archival Resource Key: ark:/67531/metadc59744

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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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  • October 7, 1953

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • April 11, 2018, 6:46 p.m.

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Thumbnail image of item number 1 in: 'Investigation of the effect of spanwise positioning of a vertically symmetric ogive-cylinder nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6 with and without a fuselage'.
Thumbnail image of item number 2 in: 'Investigation of the effect of spanwise positioning of a vertically symmetric ogive-cylinder nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6 with and without a fuselage'.
Thumbnail image of item number 3 in: 'Investigation of the effect of spanwise positioning of a vertically symmetric ogive-cylinder nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6 with and without a fuselage'.
Thumbnail image of item number 4 in: 'Investigation of the effect of spanwise positioning of a vertically symmetric ogive-cylinder nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6 with and without a fuselage'.

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Silvers, H. Norman & King, Thomas J., Jr. Investigation of the effect of spanwise positioning of a vertically symmetric ogive-cylinder nacelle on the high-speed aerodynamic characteristics of a 45 degree sweptback tapered-in-thickness wing of aspect ratio 6 with and without a fuselage, report, October 7, 1953; (digital.library.unt.edu/ark:/67531/metadc59744/: accessed April 24, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.