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Ph.D. (Engg): ON HIGH-SPEED CURVED COMPRESSION RAMP AIR INTAKES

STC Seminar Hall, Dept. of Aerospace Engineering

A scramjet, i.e., a supersonic combustion ramjet, is an air-breathing engine that enables sustained atmospheric flight in the hypersonic regime. It consists broadly of four key components: the air intake, isolator, combustor, and nozzle. The air intake and the isolator collectively comprise the compression system, which captures and conditions the freestream flow to suit the […]

Ph.D.(Engg):Elastic Wave Propagation in Textured Polycrystalline Media

Auditorium (AE 005), Department of Aerospace Engineering

The performance and reliability of structural components in advanced engineering applications, such as turbine discs in aeroengines, are critically influenced by their microstructural characteristics, particularly the crystallographic texture. Texture controls the mechanical response of a material and ultimately governs the safe life of a component. Ultrasonic non-destructive evaluation (NDE) techniques offer a powerful way to […]

Ph.D. (Engg): Aerodynamic Shape Optimization of Low Observable Air Intake Duct : A Gerlach Inspiration

Online
Hybrid Hybrid Event

Air intake system supplying air to the aircraft’s propulsion system is an important part of the aircraft. In modern military aircraft, air intake ducts are bent due to stealth and layout considerations. Due to significant contribution from rotating jet engine components to Radar Cross Section, need to inhibit direct line of sight of the Engine […]

Ph.D. (Engg) : Autorotation of Single-Winged Spinning Samaras

STC Seminar Hall, Dept. of Aerospace Engineering

Nature has consistently served as a powerful source of innovation, offering elegant and sustainable solutions to complex engineering problems. Among these, the spinning samara seed stands out as a biologically efficient system for passive aerial transport. Samaras, such as those from mahogany and Buddha coconut trees, exhibit stable autorotative descent, making them strong candidates for […]

Ph.D. (Engg) : Investigations on Elastic Deformation of Ferromagnetic Rods and Ribbons

STC Seminar Hall, Dept. of Aerospace Engineering

Bulk ferromagnetic materials exhibit Joule magnetostriction with characteristic strain magnitudes on the order of (10^{-6}) to (10^{-4}), which is often insufficient for the displacement requirements of modern soft robotic and adaptive structural systems. Ferromagnetic elastic slender structures provide a promising alternative, offering the potential for large actuation displacements under small external magnetic fields. This enhanced […]

Ph.D. (Engg) : Characterization of time-frequency behavior of flow intermittency in transitional boundary layers

STC Seminar Hall, Dept. of Aerospace Engineering

The importance of transitional flow studies can be realized from the fact that it acts as a bridge between the laminar and turbulent flows. The present work deals with the investigation of time-frequency characteristics of transitional flows and their modelling, which is presented in three parts. First, we propose a wavelet-transform based smooth detector function […]

Ph.D. (Engg) : Enhancing Precise Label Prediction and Imbalance Robustness in Multi-Label Learning

STC Seminar Hall, Dept. of Aerospace Engineering

Multi-label learning (MLL) addresses learning problems in which a single data instance may simultaneously belong to multiple semantic categories. This formulation arises naturally in many real-world applications, including image and video understanding, medical diagnosis, text categorization, and bioinformatics. In many of these settings, it is not sufficient to merely rank relevant labels higher than irrelevant […]

Ph.D. (Engg) :Studies on the Mixing Layer Between Supersonic Supersonic Co-flows

STC Seminar Hall, Dept. of Aerospace Engineering

Two supersonic streams merging together in a co-flow configuration are encountered in several engineering systems, such as high-speed propulsion devices and supersonic ejectors. The thin mixing layer that develops between the two streams is dominated by compressibility effects and is prone to shock interactions in shock-dominated flows. The convective Mach number is defined relative to […]

Ph.D. (Engg) : Development of an ultra-miniature wall-shear-stress sensor

Shear stress at the wall is a quantity of fundamental importance in wall-bounded flows. It determines skin-friction drag and the dynamics of flow separation. From an engineering standpoint, it is a key parameter which dictates the overall aerodynamic performance and structural loading of flight vehicles. Hence, there is a natural motivation for the development of […]

Ph.D. (Engg) : Turbulence Energy Cascade in Physical Space in a Turbulent Channel Flow

STC Seminar Hall, Dept. of Aerospace Engineering

A comprehensive investigation of the energy and enstrophy cascade in physical space in a turbulent channel flow is presented for four Reynolds numbers. Bandpass filtering techniques are employed to isolate scales and quantify inter-scale interactions through kinetic energy flux, enstrophy generation, and enstrophy flux. Two bandpass filter formulations used in the literature are quantitatively assessed by comparing the output. The mean energy and enstrophy cascades are shown to be predominantly local for all the Reynolds numbers. Away […]

Ph.D. (Engg) : Multi-Agent Coordination using Convex Formations and Binary Tree Structures

STC Seminar Hall, Dept. of Aerospace Engineering

Multi-agent systems are increasingly deployed in missions involving large-scale tasks with complex objectives that are beyond the capability of a single agent. Such missions demand computationally efficient coordination strategies that ensure safety, reliable operation, and ease of implementation, particularly in dynamic and uncertain environments. This thesis investigates coordination strategies in multi-agent systems, specifically addressing the […]

Ph.D. (Engg) :Experimental Investigation of Autoignition Pathways and Shock-Train Dynamics During Mode Transition in a Dual-Mode Supersonic Cavity Combustor

STC Seminar Hall, Dept. of Aerospace Engineering

Hypersonic propulsion systems capable of sustained atmospheric flight are critical enablers for future reusable launch vehicles, long-range high-speed transport, and responsive global strike platforms. Among the various air-breathing concepts, scramjet engines offer unmatched efficiency at hypersonic speeds by utilizing atmospheric oxygen and avoiding the mass penalties associated with onboard oxidizers. However, the practical realization of […]

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