Introduction of High Pressure Combustion Test Facility for Gas Turbine Engine Combustor in Korea Aerospace Research Institute
Year: 2025
Type: article
Abstract: The Korea Aerospace Research Institute (KARI) has established a high-pressure gas turbine combustor test facility to conduct research on advanced turboshaft engine using a gas generator.The test facility has been designed to provide an experimental environment that simulates actual operating conditions of the gas generator.This facility consists of an air supply system, a heating system, a test rig section, a fuel supply system, a cooling air supply system, and a cooling water supply system.The facility can operate at pressures up to 40 bara and temperatures up to 650°C.The combustion test data obtained from this test facility is expected to play a crucial role in the development of next-generation gas turbines engine combustor and contribute significantly to advancements in domestic gas turbine engine technology.초
Institution: Korea Aerospace Research Institute
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: diamond
OpenAlex ID: W4415978730