Effects of Free-Stream Reynolds Number, Engine Installation, and Model Scale on Stability Characteristics of a Translating-Spike Inlet at Mach 2.0

One of 5,158 reports in the series: NACA Research Memorandums available on this site.
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Description

Memorandum presenting the effect of free-stream Reynolds number, engine installation, and model scale on inlet stability limits and on the amplitude and frequency of buzz. The data were taken at a free-stream Mach number of 2.0 and angles of attack from 0 to 6 degrees. Results regarding free-stream Reynolds number effect, model scale, and effect of engine on stability are provided.

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23 p. : ill.

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Musial, Norman T. & Bowditch, David November 13, 1957.

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

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  • Main Title: Effects of Free-Stream Reynolds Number, Engine Installation, and Model Scale on Stability Characteristics of a Translating-Spike Inlet at Mach 2.0
  • Series Title: NACA Research Memorandums

Description

Memorandum presenting the effect of free-stream Reynolds number, engine installation, and model scale on inlet stability limits and on the amplitude and frequency of buzz. The data were taken at a free-stream Mach number of 2.0 and angles of attack from 0 to 6 degrees. Results regarding free-stream Reynolds number effect, model scale, and effect of engine on stability are provided.

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23 p. : ill.

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  • Accession or Local Control No: 71N70502
  • URL: http://hdl.handle.net/2060/19710065189 External Link
  • Report No.: NACA-RM-E57D17
  • Center for AeroSpace Information Number: 19710065189
  • Archival Resource Key: ark:/67531/metadc53172

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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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  • November 13, 1957

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  • Nov. 11, 2011, 7:22 p.m.

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  • March 13, 2019, 1:49 p.m.

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Thumbnail image of item number 1 in: 'Effects of Free-Stream Reynolds Number, Engine Installation, and Model Scale on Stability Characteristics of a Translating-Spike Inlet at Mach 2.0'.
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Musial, Norman T. & Bowditch, David. Effects of Free-Stream Reynolds Number, Engine Installation, and Model Scale on Stability Characteristics of a Translating-Spike Inlet at Mach 2.0, report, November 13, 1957; (https://digital.library.unt.edu/ark:/67531/metadc53172/: accessed November 18, 2025), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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