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Article
Visualization of incipient flow separation condition on hypersonic shock–boundary layer interaction
This article presents an investigation on a correlation relevant to flow separation during shock wave–boundary layer interaction in a hypersonic flow. The study includes experimental as well as numerical compo...
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Article
An experimental and theoretical investigation of spray characteristics of im**ing jets in impact wave regime
The current study focuses on experimentally and theoretically improving the characterization of the drop size and drop velocity for like-on-like doublet im**ing jets. The experimental measurements were made...
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Article
Regimes of spray formation in gas-centered swirl coaxial atomizers
Spray formation in ambient atmosphere from gas-centered swirl coaxial atomizers is described by carrying out experiments in a spray test facility. The atomizer discharges a circular air jet and an axisymmetric...
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Chapter and Conference Paper
Drag reduction by counterflow supersonic jet for a blunt cone in high enthalpy flows
Counterflow supersonic jet is used as a drag reduction device during the experiments in free piston driven shock tunnel, HST3. Accelerometer based force balance is employed to measure the drag force experience...
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Chapter and Conference Paper
Drag reduction by a forward facing aerospike for a large angle blunt cone in high enthalpy flows
Drag reduction studies are conducted using a flat disc tipped aerospike for a 120-degree apex angle blunt cone model in high enthalpy flows. Accelerometer based force balance is used for the drag force measure...