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Sharath Sathish

Publications and source records attributed to Sharath Sathish.

2 recordsLinked to original sources

Pramana: Fine-Tuning Large Language Models for Epistemic Reasoning through Navya-Nyaya

Large language models produce fluent text but struggle with systematic reasoning, often hallucinating confident but unfounded claims. When Apple researchers added irrelevant context to mathematical problems, LLM performance degraded by 65% Apple Machine Learning Research, exposing brittle pattern-matching beneath apparent reasoning. This epistemic gap, the inability to ground claims in traceable evidence, limits AI reliability in domains requiring justification. We introduce Pramana, a novel approach that teaches LLMs explicit epistemological methodology by fine-tuning on Navya-Nyaya logic, a 2,500-year-old Indian reasoning framework. Unlike generic chain-of-thought prompting, Navya-Nyaya enforces structured 6-phase reasoning: SAMSHAYA (doubt analysis), PRAMANA (evidence source identification), PANCHA AVAYAVA (5-member syllogism with universal rules), TARKA (counterfactual verification), HETVABHASA (fallacy detection), and NIRNAYA (ascertainment distinguishing knowledge from hypothesis). This integration of logic and epistemology provides cognitive scaffolding absent from standard reasoning approaches. We fine-tune Llama 3.2-3B and DeepSeek-R1-Distill-Llama-8B on 55 Nyaya-structured logical problems (constraint satisfaction, Boolean SAT, multi-step deduction). Stage 1 achieves 100% semantic correctness on held-out evaluation despite only 40% strict format adherence revealing that models internalize reasoning content even when structural enforcement is imperfect. Ablation studies show format prompting and temperature critically affect performance, with optimal configurations differing by stage. We release all models, datasets, and training infrastructure on Hugging Face to enable further research on epistemic frameworks for AI reasoning.

cs.AI

Wind Tunnel Testing and Modeling Implications of an Advanced Turbine Cascade

This paper describes the extensive Wind Tunnel (WT) linear cascade testing campaign carried out on a constant section turbine blade developed for low subsonic applications. Comprehensive experimental program was designed to determine the aerodynamic behaviour of this blade under a wide range of varying geometrical like Pitch to Chord Ratio, Stagger Angle and Aerodynamic like Reynolds Roughness, Mach number, Incidence angle conditions. In addition to the classical Two-Dimensional (2D) measurements, targeted Three-Dimensional (3D) surveys have been performed to complement the 2D results, allowing to draw supplementary conclusions as to the behaviour of the considered blade in three-dimensions. The performed experiments predominantly covered the transitional and beginning of a fully turbulent flow regime (maximum Re is 2.5 million). Post processing of experimental results were done in view of exploitation and judgment of some key aerodynamic aspects; parameters such as profile section load distribution, loss coefficient and flow deviation angle. Alongside with confirmation of the design targets, a parallel goal pursued in the current WT testing, was to get a more accurate idea as to the predictive capabilities of the employed CFD tools (CFX and MISES) under the basic flow condition generated in the WT. The aim was to get a global picture, as to the level of agreement that can be reached by the used design tools while accounting for the afore-mentioned design, operational variables. The obtained measurement results clearly indicated the success of the design in achieving the pre-set targets. The paper further provides a detailed discussion on the identified discrepancies, measurement versus predictions, of the key parameters at the geometric, aerodynamic design as well as off-design conditions.

physics.flu-dyn