Unsteady Oblique Interaction of a Shock Wave With a Plane Disturbance

One of 1,423 reports in the series: NACA Technical Reports available on this site.

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Description

"Analysis is made of the flow field produced by oblique impingement of weak plane disturbances of arbitrary profile on a plane normal shock. Three types of disturbance are considered: (a) sound wave propagating in the gas at rest into which the shock moves; (b) sound wave overtaking the shock from behind,(The sound wave reflects as a sound wave, and a stationary vorticity wave is produced); (c) an incompressible vorticity wave stationary in the gas ahead of the shock. The incident wave refracts as a stationary vorticity wave, and either a sound wave or attenuating pressure wave is also produced" (p. ...

Physical Description

21 p.

Creation Information

Moore, Franklin K. 1954.

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

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Titles

  • Main Title: Unsteady Oblique Interaction of a Shock Wave With a Plane Disturbance
  • Series Title: NACA Technical Reports

Description

"Analysis is made of the flow field produced by oblique impingement of weak plane disturbances of arbitrary profile on a plane normal shock. Three types of disturbance are considered: (a) sound wave propagating in the gas at rest into which the shock moves; (b) sound wave overtaking the shock from behind,(The sound wave reflects as a sound wave, and a stationary vorticity wave is produced); (c) an incompressible vorticity wave stationary in the gas ahead of the shock. The incident wave refracts as a stationary vorticity wave, and either a sound wave or attenuating pressure wave is also produced" (p. 1).

Physical Description

21 p.

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  • Accession or Local Control No: 93R21483
  • URL: http://hdl.handle.net/2060/19930092193 External Link
  • Report No.: NACA-TR-1165
  • Center for AeroSpace Information Number: 19930092193
  • Archival Resource Key: ark:/67531/metadc60543

Collections

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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).

Technical Report Archive and Image Library

This selection of materials from the Technical Report Archive and Image Library (TRAIL) includes hard-to-find reports published by various government agencies. The technical publications contain reports, images, and technical descriptions of research performed for U.S. government agencies. Topics range from mining, desalination, and radiation to broader physics, biology, and chemistry studies. Some reports include maps, foldouts, blueprints, and other oversize materials.

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Creation Date

  • 1954

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • July 30, 2018, 4:47 p.m.

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Moore, Franklin K. Unsteady Oblique Interaction of a Shock Wave With a Plane Disturbance, report, 1954; (digital.library.unt.edu/ark:/67531/metadc60543/: accessed October 21, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.