Experimental investigation of hot and cold side jet interaction with a supersonic cross-flow
Stahl, Bernhard and Emunds, Hans and Gülhan, Ali (2009) Experimental investigation of hot and cold side jet interaction with a supersonic cross-flow. Aerospace Science and Technology (13), pp. 488-496. Elsevier Masson SAS.
Full text not available from this repository.
This paper reports on experimental aerodynamic investigations on a high-speed missile with side jet control especially with regard to the interaction of cold and hot side jets with supersonic cross-flow. The hot jets were generated with solid propellants. To analyze the effect of the hot jet in relation to side jet control, wall pressure distributions were measured in the area of jet interaction. As a test parameter, the jet pressure ratio was varied and schlieren images were taken to visualize the shocks. In additon, the development of large-scale vortex structures on hot gas jets was detected with high-speed videos. The frame sequences show periodical turbulent jet structures and permit the manual evaluation of their spatial distribution. Analyzing the images, the convection velocities of the large-scale structures and their convection angles were determined. The convection velocities reach the magnitude of cross-flow velocity shortly behind the hot jet exit.
|Title:||Experimental investigation of hot and cold side jet interaction with a supersonic cross-flow|
|Journal or Publication Title:||Aerospace Science and Technology|
|In Open Access:||No|
|In ISI Web of Science:||Yes|
|Page Range:||pp. 488-496|
|Publisher:||Elsevier Masson SAS|
|Keywords:||Hot side jet, Supersonic cross flow, Large-scale structures, Convection velocities|
|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 - Military Technologies|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology|
|Deposited By:||Christine Adams|
|Deposited On:||25 Jan 2010 15:35|
|Last Modified:||07 Feb 2013 20:26|
Repository Staff Only: item control page