A Parametric Starting Study of an Axial-Centrifugal Gas Turbine Engine Using a One-Dimensional Dynamic Engine Model and Comparisons to Experimental Results: Part I—Model Development and Facility Description
暂无分享,去创建一个
Richard D. Wright | Doug Garrard | Anne Daugherty | Howard Reynolds | A. K. Owen | A. Owen | Howard Reynolds | A. Daugherty | D. Garrard
[1] R. Crawford,et al. Quantitative evaluation of transient heat transfer on axial flow compressor stability , 1985 .
[2] D. R. Pitts,et al. Elements of transport phenomena , 1972 .
[3] Gordon C. Oates. Aerothermodynamics of Gas Turbine and Rocket Propulsion , 1997 .
[4] J. P. Longwell,et al. HIGH-TEMPERATURE REACTION RATES IN HYDRO-CARBON COMBUSTION , 1955 .
[5] Doug Garrard. ATEC: The Aerodynamic Turbine Engine Code for the Analysis of Transient and Dynamic Gas Turbine Engine System Operations: Part 1 — Model Development , 1996 .
[6] Milton W. Davis,et al. A stage-by-stage post-stall compression system modeling technique: methodology, validation, and application , 1986 .
[7] Glenn Douglas Garrard,et al. ATEC: The Aerodyanmic Turbine Engine Code for the Analysis of Transient and Dynamic Gas Turbine Engine System Operations , 1995 .
[8] Milt Davis,et al. Joint Dynamic Airbreathing Propulsion Simulations Partnerships (JDAPS) , 1995 .