Verma, N and Lonkar, S and Panda, PP (2022) Reduced order model based on Gradient Optimization for Two Dimensional Scramjet Inlets. In: AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022, 3-7 Jan 2022, San Diego.
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Abstract
The optimization of the two-dimensional inlet for N ramps and M cowl has been reported. Gradient-based optimization techniques are used to minimize total pressure loss across the system of shocks. The geometry is then generated based on the optimization process. Different case studies have been taken to compare the effect of a number of ramps and cowl on the performance of the intake. The results from the code are then compared with a CFD package. As found in the previous study, for optimum conditions, the pressure rises across each ramp and each cowl were equal was reported. A quasi-one-dimensional model was formulated to design the isolator and combustor geometry for the optimized inlet. Variation of normalized pressure rise and shock train length along the length of the engine was reported at different equivalence ratios for hydrogen as fuel. © 2022, American Institute of Aeronautics and Astronautics Inc. All rights reserved.
Item Type: | Conference Paper |
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Publication: | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 |
Publisher: | American Institute of Aeronautics and Astronautics Inc, AIAA |
Additional Information: | The copyright for this article belongs to American Institute of Aeronautics and Astronautics Inc, AIAA |
Keywords: | Intake systems; Ramjet engines, Gradient optimization; Gradient-based optimization; Model-based OPC; Optimisations; Pressure rise; Reduced order modelling; Reduced-order model; Scramjet inlets; Two-dimensional; Two-dimensional inlets, Propulsion |
Department/Centre: | Division of Mechanical Sciences > Aerospace Engineering(Formerly Aeronautical Engineering) |
Date Deposited: | 13 Feb 2022 08:44 |
Last Modified: | 13 Feb 2022 08:44 |
URI: | http://eprints.iisc.ac.in/id/eprint/71359 |
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