Study on the Propagation of Inlet Flow Distortion in Axial Compressor Using an Integral Method -- Stall Prediction of In-flight Compressor due to Flaming of Refueling Leakage near Inlet -- Parametric Study of Inlet Distortion Propagation in Compressor with Integral Approach and Taguchi Method -- A Development of Novel Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor -- Parametric Study of Greitzer's Instability Flow Model Through Compressor System Using Taguchi Method
Summary
"Ĩs a book, to bring together the quick integral approaches and advances in the field for the predication of stall and surge problem in compressor. This book is useful for people involved in the flow analysis, design and testing of rotating machinery. For students, it can be used as a specialized topic of senior undergraduate or graduate study. The book can also be served as a self-study material to those who keen to acquire this knowledge."--Jacket
