Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310 and 3,500 degrees R on a magnesium fin with several leading-edge modifications

One of 5,164 reports in the series: NACA Research Memorandums available on this site.

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Description

Report presenting testing of four models of a thin magnesium fin, with the leading edge swept back 35 degrees, of a type used to stabilize the first stages of rocket-propelled multistage hypersonic models. The investigation was carried out to determine some effects of aerodynamic heating at high stagnation temperatures on the leading edges of fins and to determine the relative effectiveness of several leading-edge protective methods. The fins tested included a basic fin, a fin with a blunt leading edge, a fin with a blunt leading edge wrapped with Inconel, and a fin with a blunt leading edge made of ... continued below

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Bland, William M., Jr. & Bressette, Walter E. April 18, 1957.

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

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  • Main Title: Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310 and 3,500 degrees R on a magnesium fin with several leading-edge modifications
  • Series Title: NACA Research Memorandums

Description

Report presenting testing of four models of a thin magnesium fin, with the leading edge swept back 35 degrees, of a type used to stabilize the first stages of rocket-propelled multistage hypersonic models. The investigation was carried out to determine some effects of aerodynamic heating at high stagnation temperatures on the leading edges of fins and to determine the relative effectiveness of several leading-edge protective methods. The fins tested included a basic fin, a fin with a blunt leading edge, a fin with a blunt leading edge wrapped with Inconel, and a fin with a blunt leading edge made of stainless steel.

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  • Accession or Local Control No: 93R18947
  • URL: http://hdl.handle.net/2060/19930089657 External Link
  • Report No.: NACA-RM-L57C14
  • Center for AeroSpace Information Number: 19930089657
  • Archival Resource Key: ark:/67531/metadc63305

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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

  • April 18, 1957

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • April 12, 2018, 5:21 p.m.

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Bland, William M., Jr. & Bressette, Walter E. Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310 and 3,500 degrees R on a magnesium fin with several leading-edge modifications, report, April 18, 1957; (digital.library.unt.edu/ark:/67531/metadc63305/: accessed September 22, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.