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Uniformity of Ludwieg tube flowsPressure and speed of sound measurements are used to obtain averaged gas properties in a Ludwieg combustion tube in which the gas is burned just prior to use. Absorption of a laser beam in the exit flow is used to check the predicted temperature uniformity. The burning process and the heat transfer to the cold walls are modeled. Interferograms of Ludwieg tube boundary layers are utilized to develop a new semiempirical boundary layer expression referred to as the integral density thickness, which is then applied to a recently developed linearized analysis of the effects of this layer. Pressure-time histories are determined for a wide range of tube flow Mach number and aspect ratio. Viscous and nonviscous effects are considered. It is shown that although the influence of the integral density thickness on the flow can be large, a modified linear theory can be used to estimate the effects for arbitrary tube flow Mach number and values of the aspect ratio that include cases where the boundary layers have merged.
Document ID
19760052557
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Russell, D. A.
(Washington Univ. Seattle, WA, United States)
Knoke, G. S.
(Washington Univ. Seattle, WA, United States)
Wai, J. C.
(Washington, University Seattle, Wash., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Subject Category
Research And Support Facilities (Air)
Meeting Information
Meeting: Modern developments in shock tube research
Location: Kyoto
Country: Japan
Start Date: July 14, 1975
End Date: July 16, 1975
Accession Number
76A35523
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-73-2512
CONTRACT_GRANT: NGR-48-002-107
Distribution Limits
Public
Copyright
Other

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