Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition

One of 1,424 reports in the series: NACA Technical Reports available on this site.

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Description

Report presents the results of experimental and theoretical research conducted on flow separation associated with steps, bases, compression corners, curved surfaces, shock-wave boundary-layer reflections, and configurations producing leading-edge separation. Results were obtained from pressure-distribution measurements, shadowgraph observations, high-speed motion pictures, and oil-film studies. The maximum scope of measurement encompassed Mach numbers between 0.4 and 3.6, and length Reynolds numbers between 4,000 and 5,000,000.

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Chapman, Dean R; Kuehn, Donald M & Larson, Howard K January 1, 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 696 times , with 4 in the last month . More information about this report can be viewed below.

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  • Main Title: Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition
  • Series Title: NACA Technical Reports

Description

Report presents the results of experimental and theoretical research conducted on flow separation associated with steps, bases, compression corners, curved surfaces, shock-wave boundary-layer reflections, and configurations producing leading-edge separation. Results were obtained from pressure-distribution measurements, shadowgraph observations, high-speed motion pictures, and oil-film studies. The maximum scope of measurement encompassed Mach numbers between 0.4 and 3.6, and length Reynolds numbers between 4,000 and 5,000,000.

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  • : 93R21633
  • URL: http://hdl.handle.net/2060/19930092343 External Link
  • Report No.: NACA-TR-1356
  • Center for AeroSpace Information Number: 19930092343
  • Archival Resource Key: ark:/67531/metadc60772

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

  • January 1, 1958

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

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  • Feb. 3, 2017, 12:24 p.m.

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Citations, Rights, Re-Use

Chapman, Dean R; Kuehn, Donald M & Larson, Howard K. Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition, report, January 1, 1958; (digital.library.unt.edu/ark:/67531/metadc60772/: accessed December 15, 2017), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.