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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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)|
|Title:||A BOOT for a supersonic free jet|
|Page Range:||p. 106|
|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|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L AR - 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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