Temperature distribution and thermal stress analysis for turbojet engine turbine guide blade
Coll.of Energy and Power, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016,China;Air Force Deputy Department of Jingfeng, Beijing 100074,China;Beijing Power Generating Mechinery Inst., Beijing 100074,China;School of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083,China;School of Jet Propulsion, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083,China;Beijing Power Generating Mechinery Inst., Beijing 100074,China
