Ramraj Harikanth Sundararaj

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Publications (12)

• Performance of a turbojet engine with fluidic thrust vectoring
  The Aeronautical Journal 2022 5 citations DOI: 10.1017/aer.2022.27
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• Aerodynamic and Aero-Acoustic Performance of an Adjustable Pitch Axial Flow Fan
  Green Energy and Technology 2022 0 citations DOI: 10.1007/978-981-16-2648-7_3
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• Validating the Iterative Design Procedure for an Axial Flow Turbine Test Rig
  ASME 2021 Gas Turbine India Conference 2021 0 citations DOI: 10.1115/gtindia2021-76080
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• An Iterative Approach towards Single stage Axial Fan Design using Off Design Prediction
  Defence Science Journal 2021 0 citations DOI: 10.14429/dsj.71.16699
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• Effect of nozzle exit area on the performance of a turbojet engine
  Aerospace Science and Technology 2021 22 citations DOI: 10.1016/j.ast.2021.106844
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• Nozzle Performance Maps for Fluidic Thrust Vectoring
  Journal of Propulsion and Power 2021 15 citations DOI: 10.2514/1.b38044
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• Starting Characteristics of a Micro Gas Turbine Engine at Different Loading Conditions
  Sustainable Development for Energy, Power, and Propulsion 2021 2 citations DOI: 10.1007/978-981-15-5667-8_16
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• Analysis of Failed Startup Sequence of a Single Spool Turbojet Engine
  Volume 8: Industrial and Cogeneration; Manufacturing Materials and Metallurgy; Marine; Microturbines, Turbochargers, and Small Turbomachines 2020 0 citations DOI: 10.1115/gt2020-14778
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• Design and Development of an Engine Nozzle Testing Facility
  Volume 8: Industrial and Cogeneration; Manufacturing Materials and Metallurgy; Marine; Microturbines, Turbochargers, and Small Turbomachines 2020 0 citations DOI: 10.1115/gt2020-14779
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• Performance Simulation of an Engine Retrofitted With Thrust Vectoring Capabilities
  Volume 2: Combustion, Fuels, and Emissions; Renewable Energy: Solar and Wind; Inlets and Exhausts; Emerging Technologies: Hybrid Electric Propulsion and Alternate Power Generation; GT Operation and Maintenance; Materials and Manufacturing (Including Coat… 2019 1 citation DOI: 10.1115/gtindia2019-2448
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