Performance Calculation Of Turbo-prop

Performance calculate of aero engine has been a very important technology in its research, design, manufacture, experiment and application. In the choosing and the optimizing of cycle parameter, designing control rule and flow bypass, simulating the impetus system and integrative design of the aircraft and aero engine, it is also the basic element.By right of its mature technology,high dependability,low fuel consuming, with the fuel price durative rising, turboprop will be used broad again. It is very practical for us to analysis and calculate turboprop Performance to improve the aero engine so that we can make it take much more possession of the civil aviation market.The dissertation with a view to do a systemic research in various factor of the effect on steady and dynamic Performance, at the same time it probe into the method of the calculating for design point, co-working , steady or dynamic Performance and write the corresponding calculating program. With the structure and Performance curve of the WJ5A1 engine, validate the program, the result satisfy the requirement of the Performance analysis for turboprop design.