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Collected works of H.S. Tsien (1938-1956) /
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 hi...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
[Place of publication not identified] :
Academic Press,
2012.
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| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 100 | 1 | |a Qian, Xuesen, |d 1911-2009. | |
| 245 | 1 | 0 | |a Collected works of H.S. Tsien (1938-1956) / |c H.S. Tsien. |
| 260 | |a [Place of publication not identified] : |b Academic Press, |c 2012. | ||
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| 520 | |a 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. The author is one of the most significant Chinese scientists in the past 70 years. Focuses on a series of key problems in aerodynamics, stability of shells, rocket ballistics and engine analyses. Collects Tsien's work as author and co-author from his time working in the US. | ||
| 504 | |a Includes bibliographical references and index. | ||
| 546 | |a Includes biography and postscript in Chinese. | ||
| 505 | 0 | |a Front Cover; Collected Works of Hsue-Shen Tsien (1938-1956); Copyright Page; Contents; About this Book; Hsue-shen Tsien's Biography; Boundary Layer in Compressible Fluids; Summary; References; Supersonic Flow over an Inclined Body of Revolution; Summary; References; Problems in Motion of Compressible Fluids and Reaction Propulsion; Acknowledgements; Table of Contents; Part (I) -- Boundary Layer in Compressible Fluids; Appendix to PART (I); References on PART (I); Part (II) -- Supersonic Flow over an Inclined Body of Revolution; References on PART (II) | |
| 505 | 8 | |a Part (III) -- Application of Tschapligin's Transformation to Two Dimensional Subsonic FlowAppendix to PART (III); References on PART (III); Part (IV) -- Flight Analysis of a Sounding Rocket with Special Reference to Propulsion by Successive Impulses; References on PART (IV); Flight Analysis of a Sounding Rocket with Special Reference to Propulsion by Successive Impulse; Summary; Introduction; Notation; I; II; III; IV; References; Two-Dimensional Subsonic Flow of Compressible Fluids; Summary; Introduction; Approximation to the Adiabatic Relation; Section I; Section II; Concluding Remarks; References. | |
| 505 | 8 | |a The Buckling of Spherical Shells by External PressureGeneral Consideration; 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; Summary; Introduction; Part I; Part II; Part III; Appendix I; References. | |
| 505 | 8 | |a The Buckling of Thin Cylindrical Shells under Axial CompressionStresses 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 Column. | |
| 505 | 8 | |a Case of Two Equally Spaced SupportCase 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 Disturbance; Conclusion; References; A Theory for the Buckling of Thin Shells; Summary; 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. | |
| 650 | 0 | |a Aerospace engineering. | |
| 650 | 6 | |a A�erospatiale (Ing�enierie) |0 (CaQQLa)201-0277933 | |
| 650 | 7 | |a Aerospace engineering |2 fast |0 (OCoLC)fst00798623 | |
| 776 | 0 | 8 | |i Print version: |a Tsien, Hsue-Shen. |t Collected works of H.S. Tsien. |b 1st ed. |d Oxford : Academic Press, 2012 |z 9780123982773 |w (OCoLC)774488009 |
| 856 | 4 | 0 | |u https://sciencedirect.uam.elogim.com/science/book/9780123982773 |z Texto completo |