Experimental results from a test in rough air at high subsonic speeds of a tailless rocket model having cruciform triangular wings, and a note on the calculation of mean square loads of aircraft in continuous rough air

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

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Description

Report presenting results of testing of a rocket model with cruciform 60 degree triangular wings in continuous rough air at transonic speeds. The wing arrangement tested appears to be useful for improving the accuracy of the results. Results regarding the characteristics of the rough-air response, variation of acceleration with Mach number, and evaluation of the cruciform arrangement are provided.

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Vitale, A. James & Mitchell, Jesse L. April 13, 1956.

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

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  • Main Title: Experimental results from a test in rough air at high subsonic speeds of a tailless rocket model having cruciform triangular wings, and a note on the calculation of mean square loads of aircraft in continuous rough air
  • Series Title: NACA Research Memorandums

Description

Report presenting results of testing of a rocket model with cruciform 60 degree triangular wings in continuous rough air at transonic speeds. The wing arrangement tested appears to be useful for improving the accuracy of the results. Results regarding the characteristics of the rough-air response, variation of acceleration with Mach number, and evaluation of the cruciform arrangement are provided.

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  • Accession or Local Control No: 93R18505
  • URL: http://hdl.handle.net/2060/19930089215 External Link
  • Report No.: NACA-RM-L55L28
  • Center for AeroSpace Information Number: 19930089215
  • Archival Resource Key: ark:/67531/metadc62392

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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 13, 1956

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • April 9, 2018, 5:44 p.m.

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Vitale, A. James & Mitchell, Jesse L. Experimental results from a test in rough air at high subsonic speeds of a tailless rocket model having cruciform triangular wings, and a note on the calculation of mean square loads of aircraft in continuous rough air, report, April 13, 1956; (digital.library.unt.edu/ark:/67531/metadc62392/: accessed October 21, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.