Compressor Instability with Integral Methods
(Sprache: Englisch)
This book brings together the quick integral approaches and advances in the field for the prediction of stall and surge problems in the compressor. The book is useful for people involved in the flow analysis, design and testing of rotating machinery. For...
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Klappentext zu „Compressor Instability with Integral Methods “
This book brings together the quick integral approaches and advances in the field for the prediction of stall and surge problems in the compressor. The 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 serve as self-study material.
Inhaltsverzeichnis zu „Compressor Instability with Integral Methods “
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.
Bibliographische Angaben
- Autoren: Eddie Y.K. Ng , Ningyu Y. Liu
- 2007, 134 Seiten, Maße: 16 x 24,1 cm, Gebunden, Englisch
- Verlag: Springer
- ISBN-10: 3540724117
- ISBN-13: 9783540724117
- Erscheinungsdatum: 08.08.2007
Sprache:
Englisch
Rezension zu „Compressor Instability with Integral Methods “
"This book is intended to be a reference material mainly for aeronautical engineering senior students, graduate-level students and practitioners in the aerospace industry with the essential background of college-level physics and integral calculus.
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