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|a 9781118479360
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|a 111847936X
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|a (OCoLC)1347025983
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|a (OCoLC)on1347025983
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|a 629.132/3
|q OCoLC
|2 23/eng/20231120
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| 100 |
1 |
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|a Rathakrishnan, Ethirajan.
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| 245 |
1 |
0 |
|a Theoretical Aerodynamics
|h [electronic resource].
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| 260 |
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|a Newark :
|b John Wiley & Sons, Incorporated,
|c 2013.
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| 300 |
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|a 1 online resource (561 p.).
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| 490 |
1 |
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|a New York Academy of Sciences Ser.
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| 500 |
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|a Description based upon print version of record.
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| 500 |
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|a 4.7.1 Thickness to Chord Ratio of Symmetrical Aerofoil
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| 505 |
0 |
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|a Theoretical Aerodynamics -- Contents -- About the Author -- Preface -- 1 Basics -- 1.1 Introduction -- 1.2 Lift and Drag -- 1.3 Monoplane Aircraft -- 1.3.1 Types of Monoplane -- 1.4 Biplane -- 1.4.1 Advantages and Disadvantages -- 1.5 Triplane -- 1.5.1 Chord of a Profile -- 1.5.2 Chord of an Aerofoil -- 1.6 Aspect Ratio -- 1.7 Camber -- 1.8 Incidence -- 1.9 Aerodynamic Force -- 1.10 Scale Effect -- 1.11 Force and Moment Coefficients -- 1.12 The Boundary Layer -- 1.13 Summary -- Exercise Problems -- Reference -- 2 Essence of Fluid Mechanics -- 2.1 Introduction -- 2.2 Properties of Fluids
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| 505 |
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|a 2.2.1 Pressure -- 2.2.2 Temperature -- 2.2.3 Density -- 2.2.4 Viscosity -- 2.2.5 Absolute Coefficient of Viscosity -- 2.2.6 Kinematic Viscosity Coefficient -- 2.2.7 Thermal Conductivity of Air -- 2.2.8 Compressibility -- 2.3 Thermodynamic Properties -- 2.3.1 Specific Heat -- 2.3.2 The Ratio of Specific Heats -- 2.4 Surface Tension -- 2.5 Analysis of Fluid Flow -- 2.5.1 Local and Material Rates of Change -- 2.5.2 Graphical Description of Fluid Motion -- 2.6 Basic and Subsidiary Laws -- 2.6.1 System and Control Volume -- 2.6.2 Integral and Differential Analysis -- 2.6.3 State Equation
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| 505 |
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|a 2.7 Kinematics of Fluid Flow -- 2.7.1 Boundary Layer Thickness -- 2.7.2 Displacement Thickness -- 2.7.3 Transition Point -- 2.7.4 Separation Point -- 2.7.5 Rotational and Irrotational Motion -- 2.8 Streamlines -- 2.8.1 Relationship between Stream Function and Velocity Potential -- 2.9 Potential Flow -- 2.9.1 Two-dimensional Source and Sink -- 2.9.2 Simple Vortex -- 2.9.3 Source-Sink Pair -- 2.9.4 Doublet -- 2.10 Combination of Simple Flows -- 2.10.1 Flow Past a Half-Body -- 2.11 Flow Past a Circular Cylinder without Circulation -- 2.11.1 Flow Past a Circular Cylinder with Circulation
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| 505 |
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|a 2.12 Viscous Flows -- 2.12.1 Drag of Bodies -- 2.12.2 Turbulence -- 2.12.3 Flow through Pipes -- 2.13 Compressible Flows -- 2.13.1 Perfect Gas -- 2.13.2 Velocity of Sound -- 2.13.3 Mach Number -- 2.13.4 Flow with Area Change -- 2.13.5 Normal Shock Relations -- 2.13.6 Oblique Shock Relations -- 2.13.7 Flow with Friction -- 2.13.8 Flow with Simple T0-Change -- 2.14 Summary -- Exercise Problems -- References -- 3 Conformal Transformation -- 3.1 Introduction -- 3.2 Basic Principles -- 3.2.1 Length Ratios between the Corresponding Elements in the Physical and Transformed Planes
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| 505 |
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|a 3.2.2 Velocity Ratios between the Corresponding Elements in the Physical and Transformed Planes -- 3.2.3 Singularities -- 3.3 Complex Numbers -- 3.3.1 Differentiation of a Complex Function -- 3.4 Summary -- Exercise Problems -- 4 Transformation of Flow Pattern -- 4.1 Introduction -- 4.2 Methods for Performing Transformation -- 4.2.1 By Analytical Means -- 4.3 Examples of Simple Transformation -- 4.4 Kutta-Joukowski Transformation -- 4.5 Transformation of Circle to Straight Line -- 4.6 Transformation of Circle to Ellipse -- 4.7 Transformation of Circle to Symmetrical Aerofoil
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| 590 |
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
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| 655 |
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0 |
|a Electronic books.
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| 758 |
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|i has work:
|a Theoretical aerodynamics (Text)
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|i Print version:
|a Rathakrishnan, Ethirajan
|t Theoretical Aerodynamics
|d Newark : John Wiley & Sons, Incorporated,c2013
|z 9781118479346
|
| 830 |
|
0 |
|a New York Academy of Sciences Ser.
|
| 852 |
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