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Chapter and Conference Paper
Effect of Forward Splitter Plate Leading Edge Shape on the Cylinder Flow
Experiments have been conducted on a cylinder with a forward splitter plate at Reynolds number of 5.33 × 104. Ten different splitter plate configurations are considered wherein the leading edge of the splitter pl...
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Chapter and Conference Paper
Investigations of Density Field of a Flat Plate Shock Wave Boundary Layer Interaction at Hypersonic Speeds Using BOS
Shock wave boundary layer interaction with leading-edge bluntness problem has great effect on the performance of the aerospace vehicles. Strong interactions of the shock wave with the boundary layer lead to se...
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Chapter and Conference Paper
Studies in Free Jets from Supersonic ESTS Lobed Nozzles
The flow field associated with supersonic free jets can be understood better by using visualization techniques like schlieren in the laboratory. Supersonic jets are used in the fields of aerospace, refrigerati...
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Chapter and Conference Paper
Time Evolution of the Density Field of a Micro–Explosion Using Background Oriented Schlieren
In recent years micro-explosions have found interesting trans-disciplinary applications in the areas of food preservation,wood science, drug delivery, gene therapy and bio-medical applications [1, 2]. Generati...
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Article
Density field visualization of a Micro-explosion using background-oriented schlieren
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Chapter and Conference Paper
Density Field Measurements of a Micro–explosion Using BOS
The flow field dynamics associated with blast waves can be better understood by generating controlled micro-explosions in the laboratory. In recent years microexplosions have also found interesting trans-disci...
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Article
Density field of supersonic separated flow past an afterbody nozzle using tomographic reconstruction of BOS data
The background oriented Schlieren (BOS) technique has been applied to determine the density field in an oblique shock-separated turbulent boundary flow. Measurements were made for two cases, namely, with/witho...