全新可压缩流体气动力学讲义(英文版)(精)钱学森等9787313260666

DIVISION ONEFUNDAMENTAL PRINCIPLES
Chapter 1 Parameters in Compressible Flow
1.1 Velocity of Sound and Mach Number
1.2 Viscosity,Reynolds Number
1.3 Heat Conduction,Prandtl Number
1.4 Property of Gas,Ratio of Specific Heat
1.5 Similarity of Flows
Chapter 2 Steady One Dimensional Motion of a Perfect Compressible Fluid
2.1 Thermodynamic Relations,and Energy Equation
2.2 Perfect Gas Relations
. Flow Area,Conditions at the Throat
2.4 Flow Through a De Laval Nozzle
2.5 Pressure and Velocity Relations in Isentropic Flow
Chapter 3 Shock Wave
3.1 Relation of ntities in front and behind the Shock
3.2 Thickness of Shock
3.3 Creation of Shock from Finite Compression Disturbances
3.4 Oblique Shock
3.5 Flow over a Wedge
3.6 Pitot Tube
Appendix The Concept of Entropy and the Second Law of Thermodynamics
Chapter 4 Basic Equations of Motion of a Compressible,Inviscid and Non Heat Conducting Fluid
4.1 General Equations
4.2 Kelvin Theorem
4.3 Helmholtz Theorem
4.4 Steady Two Dimensional Rotational Flow—Detached Shock
4.5 Non steady Irrotational Flow
4.6 Method of Approximate Solution of Irrotational Subsonic Isentropic Flow
Appendix Vector Differentiation

DIVISION TWOTWO DIMENSIONAL FLOWS
Chapter 5 RayleighJanzen Method
5.1 General Equations
5.2 Solution by means of Complex Variables
5.3 Flow around a Circular Cylinder
5.4 Pressure Coefficient as a Series of Ma
5.5 Higher Order of Approximation for the Circular Cylinder
Bibliography
Chapter 6 PrandtlGlauert Method
6.1 Basic Equations for Iteration
6.2 First Approximation—PrandtlGlauert Rule
6.3 First Approximation,Using Velocity Potential
6.4 Higher Approximations
Bibliography
Chapter 7 Hodograph Method and KrmnTsien Approximation
7.1 Basic Equations in Hodograph Variables
7.2 Formulation of Problem in Hodograph Plane
7.3 Karman—Tsien Approximation
7.4 Velocity and Pressure Correction Formulae
7.5 Coordinate Correction
7.6 Application to the Flow around an Elliptic Cylinder
7.7 Further Development of Karman—Tsien Approximation
Bibliography
Chapter 8 Velocity and Pressure Correction Formulae
8.1 Correction for Boundary Effects in Subsonic Flow
8.2 Limitations of the Correction Formulae
8.3 The Recommended Correction Formulae
Bibliography
Chapter 9 Exact Solution of Isentropic Irrotational Flow
9.1 Flow with 180° Turn
9.2 Limiting Line
9.3 Breakdown of Potential Flow
9.4 General Exact Solutions
Bibliography
Chapter 10 Two Dimensional Supersonic Flows
10.1 The Lost Solution
10.2 PrandtlMeyer Flow
10.3 Flow over an Airfoil
10.4 Ackerets Formulae
10.5 Further Remarks
Bibliography
Chapter 11 Transonic and Hypersonic Similarity Laws
11.1 Transonic Flow Equation
11.2 Transonic Similarity Law
11.3 Slightly Supersonic Flow
11.4 Hypersonic Flows and Similarity Laws
Bibliography
Chapter 12 Linearized Theory of Flow over a Slender Body of Revolution
12.1 Subsonic Flows with Axial Symmetry
12.2 Linearized Subsonic Flow
1. Subsonic Flow over a Slender Ellipsoid of Revolution
12.4 Supersonic Flow over a Slender Body of Revolution
12.5 Pressure Distribution
12.6 Wave Drag
12.7 Origin of Wave Drag—Transfer of Momentum
12.8 Body of Minimum Wave Drag
12.9 Lift of a Body of Revolution
Bibliography
Appendix
Chapter 13 Non Linear Theory of Axially Symmetric Flows
13.1 Transonic Similarity Law
13.2 Hypersonic Similarity Law
13.3 "Lost Solution" of the Exact Equation
13.4 Exact Solution for Flow over a Cone
Bibliography
Chapter 14 SimilariyLwsfr Wings of Finite Span
14.1 Similarity Law in Subsonic Flow
14.2 Similarity Law in Transonic Flow
14.3 Similarity Laws in Supersonic Flow
14.4 Similarity Laws in Hypersonic Flow
Chapter 15 Rectangular Wing in Supersonic Flow
15.1 Source and Dou

钱学森，人民科学家，享誉海内外的杰出科学家和航天事业奠基人，中国近代力学事业的奠基人之一，中国系统工程理论与应用研究的倡导人，在空气动力学，航空工程，喷气推进，工程控制论，物理力学等技术科学领域作出许多开创贡献。