Introduction / 1: |
Transition Process / 1.1: |
Prediction of Transition / 1.2: |
Empirical Correlations / 1.2.1: |
Michel's Method / 1.2.2: |
Granville's Method / 1.2.3: |
H-R[subscript x] Method / 1.2.4: |
Factors that Influence Transition / 1.3: |
Effects of Freestream Turbulence and Noise / 1.3.1: |
Effects of Pressure Gradient / 1.3.2: |
Effects of Heat Transfer / 1.3.3: |
Effects of Surface Roughness / 1.3.4: |
Effects of Suction / 1.3.5: |
Effects of Surface Curvature / 1.3.6: |
References |
Stability-Transition Theory / 2: |
Underlying Mathematical Arguments for e[superscript n]-Method / 2.1: |
Linear Stability Equations / 2.3: |
Orr-Sommerfeld Equation / 2.3.1: |
Properties of the Orr-Sommerfeld Equation for Two-Dimensional Flows / 2.3.2: |
e[superscript n]-Method for Two-Dimensional Flows / 2.4: |
e[superscript n]-Method for Three-Dimensional Flows / 2.5: |
Eigenvalue Formulations / 2.5.1: |
The Zarf / 2.5.2: |
Numerical Method / 3: |
Numerical Solution of the Orr-Sommerfeld Equation for Two-Dimensional Flows / 3.1: |
Eigenvalue Procedure for Stability Diagrams / 3.2.1: |
Eigenvalue Procedure for Transition / 3.2.2: |
Numerical Solution of the Orr-Sommerfeld Equation for Three-Dimensional Flows: Mack/Arnal Eigenvalue Formulation / 3.3: |
Numerical Solution of the Orr-Sommerfeld Equation for Three-Dimensional Flows: Cebeci-Stewartson Eigenvalue Formulation / 3.4: |
Eigenvalue Procedure for Zarf / 3.4.1: |
Estimation of Eigenvalues / 3.4.2: |
Appendix 3A |
Stability Transition Program for Two-Dimensional Incompressible Flows / 4: |
Description of the Computer Program STP / 4.1: |
MAIN / 4.2.1: |
Subroutine VELPRO / 4.2.2: |
Subroutine CSAVE / 4.2.3: |
Subroutine NEWTON / 4.2.4: |
Subroutine NEWTONI / 4.2.5: |
Stability Diagrams for Falkner-Skan Flows / 4.3: |
Falkner-Skan Flows / 4.3.1: |
Sample Calculations for Constructing Stability Diagrams for Blasius Flow / 4.3.2: |
Sample Calculations for Constructing Stability Diagrams for Lower-Branch Solutions of the Falkner-Skan Equation / 4.3.3: |
Sample Calculations for Predicting Transition / 4.4: |
Flat-Plate Flow / 4.4.1: |
Airfoil Flow / 4.4.2: |
Description of the Computer Program STPW / 4.5: |
Input to STPW / 4.5.1: |
Sample Calculations / 4.5.2: |
Shooting Method / Appendix 4A: |
Description of the Method for f"[subscript w greater than or equal] 0 / 4A.1: |
Description of the Method for f"[subscript w less than sign] 0 / 4A.2: |
Computer Program / 4A.3: |
An Interactive Boundary-Layer and Stability-Transition Program for Two-Dimensional Flows / 5: |
Interactive Boundary-Layer Method / 5.1: |
Turbulence Model / 5.2.1: |
Inviscid Method / 5.2.2: |
Extension of the Interactive Boundary-Layer and Stability-Transition Approach to Multielement Airfoils / 5.2.4: |
Airfoils at High Reynolds Numbers / 5.4: |
Accuracy of the e[superscript n]-Method for Flows with Separation / 5.5: |
Airfoils at Low Reynolds Numbers / 5.6: |
Multielement Airfoils / 5.7: |
Stability-Transition Program for Three-Dimensional Incompressible Flows / 6: |
Description of the Computer Program 3DSTP and Sample Calculations / 6.1: |
Description of the Computer Program / 6.2.1: |
Applications of 3DSTP / 6.2.2: |
ONERA-D Infinite Swept Wing / 6.3.1: |
Prolate Spheroid / 6.3.2: |
Prediction of Transition with Curvature Effect / 6.4: |
Stability Equations with Curvature Terms / 6.4.1: |
Calculation of the Curvature Terms / 6.4.2: |
Effects of Sweep Angle and Reynolds Number on Transition with Curvature Effect Included in the Stability Equations / 6.4.3: |
Computer Program 3DSTPWC and Sample Calculations / 6.5: |
Description of Input / 6.5.1: |
A Stability-Transition Program for Three-Dimensional Compressible Flows on Wings / 6.5.2: |
Boundary-Layer Equations / 7.1: |
Initial Conditions / 7.3: |
Quasi-Three-Dimensional Boundary-Layer Equations / 7.3.1: |
Attachment Line Equations / 7.3.2: |
Interface Program / 7.4: |
Choice of the Surface Coordinate System / 7.5.1: |
Geometric Parameters of the Coordinate System / 7.5.2: |
Calculation of Inviscid Velocity Components for Boundary-Layer Grid / 7.5.3: |
Solution of the Boundary-Layer Equations / 7.5.4: |
Transformed Equations / 7.6.1: |
Solution of the Stability Equations for Compressible Flows / 7.6.2: |
AS409 Infinite Swept Wing / 7.8: |
Experimental Data / 7.8.1: |
Calculations with the Mack-Arnal Formulation / 7.8.2: |
Calculations with the Cebeci-Stewartson Formulation / 7.8.3: |
Software for Calculating Transition in Incompressible and Compressible Flows on Wings with and without Suction / 7.9: |
Boundary Layer Program / 7.9.1: |
Calculation of Zarf / 7.9.2: |
Amplification Calculations / 7.9.3: |
Summary of Transition Calculations / 7.9.4: |
Calculation of the Lower Branch of the Zarf / 7.9.5: |
Amplification Calculations for Disturbances from the Lower Branch / 7.9.6: |
Amplification Calculations for Disturbances from the Upper Branch / 7.9.7: |
Transition Prediction by Parabolized Stability Equations / 8: |
Parabolized Stability Equations / 8.1: |
Subroutine START / 8.3: |
Subroutine COEF / 8.4.2: |
Subroutine GETNA / 8.4.3: |
Solution Algorithm: Subroutines MATRIX6, GAUSS, USOLV, GAMSV / 8.4.4: |
Sample Calculations with PSE / 8.5: |
Computer Programs in the CD-ROM Accompanying the Book / Appendix A: |
Shooting Method: For f"(0) [greater than or equal] 0 / A.1: |
Shooting Method: For f"(0) [less than sign] 0 / A.2: |
2D Stability Transition Program (STP2D) / A.3: |
Interactive Boundary-layer (IBL) Program / A.4: |
Panel Method (HSPM), 2D Interface Program (IPRPM2D), Inverse Boundary-Layer Program (INBLP) and STP2D / A.5: |
HSPM, IPRPM2D, Boundary-Layer Infinite Swept Wing (BLISW) Program and 3D Stability-Transition Program (3DSTP) / A.6: |
Stability-Transition Program Based on Parabolized Stability Equations (PSE) / A.7: |
Cross-Flow Dominated Flows / A.7.1: |
Flows in Which Tollmien-Schlichting (T-S) Waves Dominate / A.7.2: |
Computer Programs in the CD-ROM Available from the Author / Appendix B: |
Boundary Layer and Stability-Transition Program for Air, Water and Sea (STPW) / B.1: |
Panel Method (HSPM), 2D Interface Program (IPRPM), Infinite Swept Wing Boundary-Layer Program (BLISW) and 3D Stability Transition Program with Curvature Effects (3DSTPWC) / B.2: |
HSPM, IPRPM, BLISW, 3DSTPWC, Parabolized Stability Equations (PSE) / B.3: |
Flows in Which Tollmien-Schlichting (T-S) Instability Dominates / B.3.1: |
Interactive Boundary-Layer Method for Single and Multielement Airfoils (MEIBL) / Appendix C: |
Application of MEIBL to Three-Dimensional Flows / C.1: |
Inviscid Flow / C.1.1: |
Viscous Flow / C.1.2: |
Interaction / C.1.3: |
Coordinate Systems for Viscous and Inviscid Flow Calculations / C.2: |
User's Manual / C.3: |
Input Data / C.3.1: |
Output Data / C.3.2: |
Detailed Flow at [alpha] = 4[degree] and [alpha] = 20[degree] / C.4: |
Force and Moment Coefficient Calculations / C.4.2: |
Software for Calculating Transition in Three-Dimensional Compressible Flows / Appendix D: |
Description of the Boundary Layer Program / D.1: |
Input Data Description / D.1.1: |
Output Data Description / D.1.2: |
Description of the Transition Calculation Procedure / D.2: |
Zarf Calculation / D.2.1: |
Amplification Calculation / D.2.2: |
Summary of the Procedure / D.2.3: |
Sample Calculation: Input and Output Data Description / D.3: |
Input File Description / D.3.1: |
Zarf Upper Branch Calculation / D.3.2: |
Quick Reference Manual / D.3.5: |
Subject Index |
Introduction / 1: |
Transition Process / 1.1: |
Prediction of Transition / 1.2: |