Tables and charts of flow parameters across oblique shocks

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Description

Shock-wave equations have been evaluated for a range of Mach number in front of the shock from 1.05 to 4.0. Mach number behind the shock, pressure ratio, derivation of flow, and angle of shock are presented on charts. Values are also included for density ratio and change in entropy.

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44 p. : ill., tables ; 28 cm.

Creation Information

Neice, Mary M. August 1948.

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This report is part of the collection entitled: Technical Report Archive and Image Library 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 5731 times , with 168 in the last month . More information about this report can be viewed below.

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Description

Shock-wave equations have been evaluated for a range of Mach number in front of the shock from 1.05 to 4.0. Mach number behind the shock, pressure ratio, derivation of flow, and angle of shock are presented on charts. Values are also included for density ratio and change in entropy.

Physical Description

44 p. : ill., tables ; 28 cm.

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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.

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

  • August 1948

Added to The UNT Digital Library

  • Sept. 25, 2014, 8:32 p.m.

Description Last Updated

  • Oct. 25, 2017, 9:09 a.m.

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Neice, Mary M. Tables and charts of flow parameters across oblique shocks, report, August 1948; Washington D.C.. (https://digital.library.unt.edu/ark:/67531/metadc172508/: accessed March 21, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.