Some effects of Reynolds number on the stability of a series of flared-body and blunted-cone models at Mach numbers from 1.62 to 6.86

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Description

Report discussing an investigation of the stability of a series of flared-body and blunted-cone models at a range of Mach numbers. Increasing the flare length was found to increase static stability and the damping in pitch. The Reynolds number was found to have a large effect on static stability at lower Mach numbers, but little effect on the higher end of the range covered in testing.

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Kehlet, Alan B. January 7, 1958.

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

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  • Main Title: Some effects of Reynolds number on the stability of a series of flared-body and blunted-cone models at Mach numbers from 1.62 to 6.86
  • Series Title: NACA Research Memorandums

Description

Report discussing an investigation of the stability of a series of flared-body and blunted-cone models at a range of Mach numbers. Increasing the flare length was found to increase static stability and the damping in pitch. The Reynolds number was found to have a large effect on static stability at lower Mach numbers, but little effect on the higher end of the range covered in testing.

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  • Accession or Local Control No: 71N70831
  • URL: http://hdl.handle.net/2060/19710065518 External Link
  • Report No.: NACA-RM-L57J29
  • Center for AeroSpace Information Number: 19710065518
  • Archival Resource Key: ark:/67531/metadc53192

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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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  • January 7, 1958

Added to The UNT Digital Library

  • Nov. 11, 2011, 7:22 p.m.

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  • April 12, 2018, 5:23 p.m.

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Thumbnail image of item number 1 in: 'Some effects of Reynolds number on the stability of a series of flared-body and blunted-cone models at Mach numbers from 1.62 to 6.86'.
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Thumbnail image of item number 3 in: 'Some effects of Reynolds number on the stability of a series of flared-body and blunted-cone models at Mach numbers from 1.62 to 6.86'.
Thumbnail image of item number 4 in: 'Some effects of Reynolds number on the stability of a series of flared-body and blunted-cone models at Mach numbers from 1.62 to 6.86'.

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Kehlet, Alan B. Some effects of Reynolds number on the stability of a series of flared-body and blunted-cone models at Mach numbers from 1.62 to 6.86, report, January 7, 1958; (digital.library.unt.edu/ark:/67531/metadc53192/: accessed April 21, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.