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A BOOT for a supersonic free jet

Rein, M. and Meier, G.E.A. and Raffel, M, and Richard, H. (1999) A BOOT for a supersonic free jet. 52nd Annual Meeting of the Division of Fluid Dynamics of the.

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Abstract

A new optical method for determining the density within a flow field will be introduced. The method that has been called BOOT is particularly simple. In order to demonstrate the capabilities of BOOT a supersonic free jet exiting a planar nozzle has been observed both by BOOT and by a shadowgraph method. The results obtained with both methods will be compared. In the example shown the exit Mach number of the jet is about M = 2.5 and the stagnation temperature was chosen such that the temperature in the jet matches approximately the temperature of the ambient air.

Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=2003,
Title:A BOOT for a supersonic free jet
Authors:
AuthorsInstitution or Email of Authors
Rein, M.UNSPECIFIED
Meier, G.E.A.UNSPECIFIED
Raffel, M, UNSPECIFIED
Richard, H.UNSPECIFIED
Date:1999
Page Range:p. 106
Status:Published
Keywords:schlieren method, flow visualization
Event Title:52nd Annual Meeting of the Division of Fluid Dynamics of the
Organizer:American Physical Society
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: elib DLR-Beauftragter
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 19:18

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