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Two-dimensional irrotational mixed subsonic and supersonic flow of a compressible fluid and the upper critical Mach number

Tsien, Hsue-Shen and Kuo, Yung-Huai (1945) Two-dimensional irrotational mixed subsonic and supersonic flow of a compressible fluid and the upper critical Mach number. National Advisory Committee on Aeronautics , Washington, DC. http://resolver.caltech.edu/CaltechAUTHORS:20140805-133252590

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Abstract

The problem of flow of a compressible fluid past a body with subsonic flow at infinite is formulated by the hodograph method. The solution in the hodograph plane is first constructed about the origin by superposition of the particular integrals of the transformed equations of motion with a set of constants which would determine, in the limiting case, a known incompressible flow. This solution is then extended outside the circle of convergence by analytic continuation.


Item Type:Report or Paper (Technical Report)
Related URLs:
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http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19930090567.pdfOrganizationArticle
Additional Information:No copyright.
Other Numbering System:
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NACA Technical Note995
Record Number:CaltechAUTHORS:20140805-133252590
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20140805-133252590
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:47996
Collection:CaltechAUTHORS
Deposited By: George Porter
Deposited On:05 Aug 2014 22:04
Last Modified:13 Feb 2019 18:02

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