Hybrid Wave Rotor Electric Aero Propulsion

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Nalim_2014_HyWvRtr.pdf (700.31 KB)
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Date
2014
Authors
Nalim, M. Razi
Bane, Sally P.M.
Khan, M. Javed
Jagannath, Ravichandra
Language
American English
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Abstract

Purpose: The goal of this project was to investigate the proposed hybrid wave-rotor electric aero-propulsion concept (HyWREAP). The tasks were to perform flow and combustion analysis of the pressure-gain, wave-rotor combustor (WRC) turbine concept, and investigate benefits for the most likely flight application of HyWREAP.

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Keywords
Hybrid wave-rotor electric aero-propulsion concept (HyWREAP), Hybrid propulsion, Airplanes, Combustion turbine engines, Wave rotor combustion turbine (WRCT)
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Cite As
Nalim, M. Razi. (2014). Hybrid Wave-Rotor Electric Aero-Propulsion (HyWREAP). Presented at the 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
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https://hdl.handle.net/1805/20981
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Mechanical and Energy Engineering Works
Razi Nalim