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Dr. H. S. Tsien (also known as Dr. Qian Xuesen), is celebrated as the leader of the research that produced China's first ballistic missiles, its first satellite, and the Si… Read more
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Immediately download your ebook while waiting for your print delivery. No promo code needed.
Dr. H. S. Tsien (also known as Dr. Qian Xuesen), is celebrated as the leader of the research that produced China's first ballistic missiles, its first satellite, and the Silkworm anti-ship missile.
This volume collects the scientific works of Dr. H. S. Tsien (also known as Dr. Qian Xuesen) and his co-authors, which published between 1938—1956 when he was studying and working in the United States as a graduate student, scientist and professor, when aeronautic exploration stepped up from low speed to high speed regimes and astronautic technology entered its infant stage.
About This Book
Hsue-Shen Tsiens Biography
Boundary Layer in Compressible Fluids
I
II
References
Supersonic Flow over an Inclined Body of Revolution
References
Problems in Motion of Compressible Fluids and Reaction Propulsion
PART (I). Boundary Layer in Compressible Fluids
Boundary Layer in Compressible Fluids
PART (II). Supersonic Flow over an Inclined Body of Revolution
Supersonic Flow over an Inclined Body of Revolution
PART (III). Application of Tschapligin’s Transformation to Two Dimensional Subsonic Flow
Application of Tschapligin’s Transformation to Two Dimensional Subsonic Flow
PART (IV). Flight Analysis of a Sounding Rocket with Special Reference to Propulsion by Successive Impulses
Flight Analysis of a Sounding Rocket with Special Reference to Propulsion by Successive Impulses
Flight Analysis of a Sounding Rocket with Special Reference to Propulsion by Successive Impulses
Introduction
Notation
I
II
III
IV
Conclusion
References
Two-Dimensional Subsonic Flow of Compressible Fluids
Introduction
Approximation to the Adiabatic Relation
Section I
Section II
Concluding Remarks
References
The Buckling of Spherical Shells by External Pressure*
General Considerations
The Energy Expression and the Equation of Equilibrium for a Spherical Segment Under Uniform External Pressure
Approximate Solution by the Rayleigh-Ritz Method
Application to the Buckling Problem. Comparison with the Experiment
References
The Influence of Curvature on the Buckling Characteristics of Structures
Section I
Section II
Section III
Concluding Remarks
References
A Method for Predicting the Compressibility Burble
Introduction
Part I
Part II
Part III
Appendix 1
References
The Buckling of Thin Cylindrical Shells under Axial Compression
Stresses in the Median Surface and the expression for the Total Energy of the System
Calculation of the Total Energy
Relation Between the compression Stress and the Amplitude of Waves
The Relation Between the Compression Stress and the Shortening of the Shell in the Axial Direction
The Effect of the Elastic Characteristic of the testing Machine on the Buckling Phenomenon
Conclusions
References
Buckling of a Column with Non-Linear Lateral Supports
Introduction
General Theory for Straight Columns
Case of Two Equally Spaced Supports
Case of a Single Lateral Support, Effect of Initial Deflection
Case of a Single Lateral Support, Effect of Elasticity of the Testing Machine
Stability of the Equilibrium Positions Under Infinitesimal Disturbances
Conclusions
References
A Theory for the Buckling of Thin Shells
Introduction
The Criterions for Buckling
Column with a Nonlinear Elastic Lateral Support
Thin Uniform Cylindric Shell Under Axial Compression
Spherical Shells under External Pressure
Concluding Remarks
References
Heat Conduction across a Partially Insulated Wall
On the Design of the Contraction Cone for a Wind Tunnel
Formulation of the Problem
Solution of the Problem
The Results
References
Symmetrical Joukowsky Airfoils in Shear Flow
1. Problem
2. Method of solution
3. Shear flow over a circular cylinder
4. Force and moment
5. Symmetrical Joukowsky airfoils
6. Strength of circulation
7. Strengths of doublets and quadruplets
8. Lift and moment coefficients
9. Aerodynamic center
References
The “Limiting Line” in Mixed Subsonic and Supersonic Flow of Compressible Fluids
Criterion for the Breakdown of Isentropic Irrotational Flow
Axially Symmetric Flow
The Limiting Line
Limiting Hodograph and the Streamlines
Envelope of Characteristics in Hodograph Plane and Lines of Constant Velocity in Physical Plane
The Lost Solution
Continuation of Solution Beyond The Limiting Line
General Three-Dimensional Flow
References
Loss in Compressor or Turbine due to Twisted Blades
Problem
The Vortex System and the Induced Velocity
The General Blade Equation
Application I
Application II
Appendix
REFERENCE
Lifting-Line Theory for a Wing in Non-uniform Flow*
1. Introduction
2. General theory of a lifting line
3. Conditions far downstream
4. Minimum induced drag
5. Flow with velocity varying in the direction of span only
References
Atomic Energy
Introduction
The Equivalence of Energy and Mass
Atomic Structure
Nuclear Reactions
Nuclear Structure — Binding Energy
Energy Production in the Stars
Nuclear Fission — Chain Reaction
Engineering Approach to the Nuclear Reaction
References
Two-Dimensional Irrotational Mixed Subsonic and Supersonic Flow of a Compressible Fluid and the Upper Critical Mach Number
Introduction
Notations
Part I. Differential Equations of Compressible Flow and Properties of Their Particular Solutions
2. Transformation of the Differential Equations
3. The Particular Solutions of the Differential Equations
4. The Properties of the Hypergeometric Functions of Large Order
Part II. Construction of the Solutions for Compressible Flow Around a Body
6. The Functions for Incompressible Flow
7. Conformal Mapping of Incompressible Flow on the Hodograph Plan
8. Construction of a Solution about the Origin
9. Analytic Continuation of the Solution Branch Point or Order 1
10. Continuation Logarithmic Singularity
11. Transition to Physical Plane
Part III. Improvement of the Convergence of Solution by the Asymptotic Properties of Hypergeometric Functions
13. Asymptotic Solutions of the Hypergeometric Equations
14. The Asymptotic Representation of F(av, bv; cv; τ) and F(av + β, bv + β; cv; τ)
15. Transformation of the Function W(w; τ) Branch Point of Order 1
16. Continuation: Lo garithmic Singularity
17. The Coordinate Functions x (q, θ) and y (q, θ)
Part IV. Criteria for the Upper Critical Mach Number
19. The Condition for the Limiting Line
20. The Approximate Determination of the Upper Critical Mach Number
Part V. Application — Elliptic Cylinders
22. The Functions z0(w), W0 (w) and Λ0 (w)
23. Expansions of W0 (w) and Λ0 (w)
24. The Stream Function ψ(q, θ)
25. The Coordinate Functions x(q, θ) and y(q, θ)
Conclusions
References
Appendix A Proof of Theorem (52)
Appendix B Proof of Theorem (88)
Appendix C Proof of Theorem (98)
Tables of the Hypergeometric Functions
Superaerodynamics, Mechanics of Rarefied Gases
Introduction
Mean Free Path and Realms of Fluid Mechanics
Stresses and Boundary Conditions in Slip Flow
Boundary Conditions for Slip Flows of Small Mach Number
Slip Flows at Small Mach Numbers
Free Molecule Flows at Small Mach Numbers
Free Molecule Flow at Large Mach Numbers
Free Molecule Flow Over an Inclined Plate
References
Propagation of Plane Sound Waves in Rarefied Gases
1. Introduction
2. Symbols
3. Basic Equations
4. Solution of the Differential Equations
5. Numerical Calculation
6. Results
References
Similarity Laws of Hypersonic Flows
Introduction
Differential Equation for Hypersonic Flows
Similarity Laws in Two-Dimensional Flow
Axially Symmetrical Flows
References
One-Dimensional Flows of a Gas Characterized by van der Waals Equation of State*
Introduction
Isentropic Expansion of a van der Waal Gas
Expansion in a Nozzle
Shock Wave in Supersonic Flow
Parameters for Constants a and b
Properties of Air
Tabulation of Functions for Air
Application of Results to a Hypersonic Wind Tunnel
References
Corrections on the Paper “One-Dimensional Flows of a Gas Characterized by van der Waals Equation of State”
Flow Conditions near the Intersection of a Shock Wave with Solid Boundary
1. Introduction
2. Basic Equations
3. Relations of Quantities on the Two Sides of Shock
References
Lower Buckling Load in the Non-Linear Buckling Theory for Thin Shells
Rockets and Other Thermal Jets Using Nuclear Energy: With a General Discussion on the Use of Porous Pile Materials
1. Simple Theory of Space Rockets
2. Relativistic Theory of Space Rockets
3. Idealized Optimum Design using Nuclear Energy
4. Nuclear Energy Rocket
5. Specific Examples of Nuclear Energy Rocket
6. Possibilities of Reducing the Critical Size
7. Application of Nuclear Fuel to other Thermal Jets
8. Advantages of Using Porous Pile Material
References
Engineering and Engineering Sciences*
Introduction
Contributions of an Engineering Scientist to Engineering Development
The Feasibility of a Proposal—Long Range Rockets
Rocket Propellants
Best Method of Attack— Manufacture of Fissionable Material
Reason and Remedy for a Failure — the Tacoma Narrows Bridge
Unification—Basic Research in Engineering Science
Training of an Engineering Scientist
Concluding Remarks
References
On Two-Dimensional Non-steady Motion of a Slender Body in a Compressible Fluid
1. Introduction
2. General formulation of the problem
3. Introduction of parameters
4. Theory of small perturbations
5. Further simplification in special cases
6. Influence of wind tunnel walls
7. The Case of Large Pressure Disturbance
8. The Transonic case with M1= 1
References
Wind-Tunnel Testing Problems in Superaerodynamics
Introduction
(1) Tunnel Design
(2) Flow Measurement
(3) Hot-Wire Anemometer
(4) Parameters of Flow
Appendix
References
Airfoils in Slightly Supersonic Flow
Introduction
Oblique Shock
Prandtl-Meyer Expansion
Flat Plate Airfoil
Asymmetric Wedge Airfoil
References
Interaction between Parallel Streams of Subsonic and Supersonic Velocities*
Introduction
Incident Wave
Inclined Wall
Numerical Results and Discussion
References
Appendix
Research in Rocket and Jet Propulsion*
Variable Stress
Heat Transfer
Wall-Temperature Effects
Long-Range Trajectory
References
A Generalization of Alfrey’s Theorem for Visco-elastic Media
1. Introduction
2. First boundary value problem
REFERENCE
Instruction and Research at the Daniel and Florence Guggenheim Jet Propulsion Center
Jet-Propulsion Centers
Instruction and Research of Jet Propulsion
Characteristics of Rocket and Jet-Propulsion Engineering
Material Problems
Heat Transfer
Combustion
Performance of Rocket and Jet-Propelled Vehicles
References
Influence of Flame Front on the Flow Field
Flame Front
Production of Vorticity by Flame
Flame Width in a Uniform Channel
Effect of Compressibility on Flame Width
Appendix
References
Optimum Thrust Programming for a Sounding Rocket
Formulation of the Problem
Quadratic Drag Law
Linear Drag Law
Discussion of Results
Acknowledgment
References
The Emission of Radiation from Diatomic Gases. III. Numerical Emissivity Calculations for Carbon Monoxide for Low Optical Densities at 300K and Atmospheric Pressure
I. Introduction
II. Summary of Theoretical Relations
III. Representative Emissivity Calculations for CO at 300K
IV. Limits of Validity of the Treatment for Nonoverlapping Rotational Lines for CO17
V. Approximate Emissivity Calculations for Diatomic Molecules with Nonoverlapping Rotational Lines
VA Emissivity Calculations for CO at 300K for Nonoverlapping Rotational Lines, Assuming Equal Spacing and Intensity of Lines
VB Emissivity Calculations for CO at 300K for Nonoverlapping Rotational Lines Using Asymptotic Expressions for the Modified Bessel Functions
Appendix
References
The Transfer Functions of Rocket Nozzles
Flow Conditions
Formulation of the Problem in Nozzle
Solution for Small Frequency
Solution for Large Frequencies
Concluding Remarks
References
A Similarity Law for Stressing Rapidly Heated Thin-Walled Cylinders
Stresses and Strains of a Thin-Walled Cylinder
Nondimensional Quantities and Equations of Equilibrium
Infinite Cylinder Under Uniform Internal Pressure
Linearized Theory for General Secondary Loading
Similarity Law for General Loading
Example of Dimensioning the Equivalent Cold Cylinder
Junction Stress Between Cylinder and Head
Ring Stiffener Around Cylinder
References
On the Determination of Rotational Line Half-Widths of Diatomic Molecules*
I. Introduction
II. Calculation of Rotational Half-Widths from Experimental Data
References
Automatic Navigation of a Long Range Rocket Vehicle
Equations of Motion
Normal Flight Path
Disturbance Equations
Adjoint Functions for Range Correction
Cut-Off Condition
Condition for Automatic Navigation
Discussion
Appendix
References
A Method for Comparing the Performance of Power Plants for Vertical Flight
General Relation
Applications
Detail Improvement of Rocket Engine
References
Servo-Stabilization of Combustion in Rocket Motors
Time Lag in Combustion
Intrinsic Instability
System Dynamics with Servo Control
Instability Without Servo Control
Complete Stability with Servo Control
Stability Criteria
Concluding Remarks
Appendix
References
Physical Mechanics, A New Field in Engineering Science
Basic Concepts
Physical Mechanics as an Engineering Science
Use of Approximate Models
A Question of Methodology
Concluding Remarks
References
The Properties of Pure Liquids
Lennard-Jones and Devonshire Theory of Liquids
Specific Heat at Constant Volume
Thermal Expansion and Compressibility
Specific Heat at Constant Pressure
Liquid Metals
Velocity of Sound
Transport Properties
Thermal Conductivity
Concluding Remarks
Appendix
References
Similarity Laws for Stressing Heated Wings
Introduction
Basic Equations for Heated Plate
Plateat Constant Temperature
Similarity Laws for Solid Thin Wings
Alternate Test Procedure for Thin Solid Wings
Box Wing
Discussion
Appendix—Young’s Modulus Profile
References
Take-Off from Satellite Orbit
Basic Equations
Radial Thrust
Circumferential Thrust
Discussion
References
Analysis of Peak-Holding Optimalizing Control
Introduction
Principle of Operation
Formulation of the Mathematical Problem
First-Order Input and Output Groups
Design Charts
Concluding Remarks
Appendix
References
The Poincaré-Lighthill-Kuo Method
I. Introduction
II. Ordinary Differential Equations
III. Hyperbolic Partial Differential Equations
IV. Elliptic Partial Differential Equations
V. Applications to Fluid Boundary Layer Problems
VI. Concluding Remarks
References
Thermodynamic Properties of Gas at High Temperatures and Pressures
1. Equation of States of Dense Gas
2. Lennard-Jones and Devonshire Theory
3. Other Thermodynamic Functions
References
Thermonuclear Power Plants
1. Introduction
2. Thermonuclear Reaction Rate
3. Example: Deuterium Reaction
4. Thermonuclear Reaction Chamber
5. Thermonuclear Power Station
6. Ignition
7. Thermonuclear Power Industry
References
Index
TH