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Compression Shocks in Two-Dimensional Gas FlowsThe following are arguments on the compression shocks in gas flow start with a simplified representation of the results of the study made by Th. Meyer as published in the Forschungsheft 62 of the VDI, supplemented by several amplifications for the application.In the treatment of compression shocks, the equation of energy, the equation of continuity, the momentum equation, the equation of state of the particular gas, as well as the condition Of the second law of thermodynamics that no decrease of entropy is possible in an isolated system, must be taken into consideration. The result is that, in those cases where the sudden change of state according to the second law of thermodynamics is possible, there always occurs a compression of the gas which is uniquely determined by the other conditions.
Document ID
20050029423
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Busemann, A.
Date Acquired
August 22, 2013
Publication Date
February 1, 1949
Publication Information
Publication: Vortraege aus dem Gebiete der Aerodynamik und Verwandter Gebiete
Subject Category
Numerical Analysis
Report/Patent Number
NACA-TM-1199
Report Number: NACA-TM-1199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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