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Purchase Benefits
What is included with this book?
Reviews | p. XI |
Foreword | p. XVII |
About this Book | p. XVII |
Methods Used in this Book | p. XVII |
Research Application | p. XVIII |
Acknowledgments | p. XVIII |
Briefly Introduction of Software: FASTFLO | p. XIX |
References | p. XX |
List of Publications Related to this Book | p. XX |
Nomenclature | p. XXI |
Study on the Propagation of Inlet Flow Distortion in Axial Compressor Using an Integral Method | p. 1 |
Introduction | p. 1 |
Theoretical Formulation | p. 3 |
Velocity and Pressure | p. 4 |
Forces | p. 5 |
Distorted Region | p. 7 |
Undistorted Region | p. 8 |
Entire Region | p. 9 |
Integral Equations | p. 10 |
Numerical Method | p. 11 |
Equations | p. 11 |
4th-order Runge-Kutta Equations | p. 11 |
Results and Discussion | p. 13 |
Previous Results | p. 13 |
Further Asymptotic Behavior Results | p. 17 |
Mass Flow Rate | p. 20 |
Critical Distortion Line | p. 22 |
Compressor Performance and Characteristic | p. 23 |
Concluding Remarks | p. 26 |
References | p. 26 |
Fortran Program: Integral Method | p. 28 |
Fortran Program: Critical Distortion Line | p. 35 |
Stall Prediction of In-flight Compressor due to Flamming of Refueling Leakage near Inlet | p. 41 |
Introduction | p. 41 |
Inlet Flow Condition | p. 42 |
Computational Domain | p. 43 |
Application of Critical Distortion Line | p. 45 |
Application of Integral Method | p. 46 |
Compressor Characteristics | p. 50 |
Effects of Rotor Blade Speed ([sigma]) | p. 52 |
Effects of Inlet Distorted Region Size ([xi](0)) | p. 53 |
Concluding Remarks | p. 55 |
References | p. 56 |
Parametric Study of Inlet Distortion Propagation in Compressor with Integral Approach and Taguchi Method | p. 57 |
Introduction | p. 57 |
Methodology | p. 59 |
Results and Analysis | p. 60 |
Case study 1: Drag-to-lift Ratio, K, is Varied | p. 64 |
Case study 2: X-axis Inlet Distorted Velocity Coefficient, [alpha](0), is Varied | p. 68 |
Case Study 3: Inlet Flow Angle, [theta subscript 0], is Varied | p. 72 |
Conclusion | p. 74 |
References | p. 75 |
A Development of Novel Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor | p. 77 |
Introduction | p. 77 |
Theoretical Formulation | p. 79 |
Results and Discussion | p. 86 |
Lift and Drag Coefficients | p. 86 |
Inlet Distorted Velocity Coefficient | p. 87 |
Inlet Incident Angle | p. 88 |
Propagation of Distortion Level | p. 91 |
Compressor Characteristics | p. 96 |
Argument for Airfoil Characteristics | p. 99 |
Concluding Remarks | p. 99 |
References | p. 100 |
Fortran Program: Chebyshev Curve Fitting | p. 101 |
Parametric Study of Greitzer's Instability Flow Model Through Compressor System Using Taguchi Method | p. 107 |
Introduction | p. 107 |
Mathematical Model | p. 108 |
Numerical Methods | p. 110 |
Results and Discussion | p. 114 |
Analysis for Case 1: with Parameters B, G and K | p. 115 |
Analysis for Case 2: with Parameters B, G and LC | p. 118 |
Summary: Parameters B, G, K and LC | p. 120 |
Conclusion | p. 121 |
References | p. 121 |
Programing: Greitzer's Model | p. 123 |
Index | p. 131 |
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