錢學森文集(錢學森文集(英文版))

錢學森文集

錢學森文集(英文版)一般指本詞條

《錢學森文集》是2011年10月1日上海交通大學出版社出版的圖書。本書介紹了錢學森解決了其中一系列關鍵問題,包括空氣動力學、殼體穩定性、火箭彈道和發動機分析等。

基本介紹

  • 書名:錢學森文集
  • 原版名稱:collected works of hsue-shen tsien
  • ISBN:9787313068309
  • 頁數:881頁
  • 出版社:上海交通大學出版社
  • 出版時間:2011年10月1日
  • 裝幀:精裝
  • 開本:16
內容簡介,目錄,

內容簡介

《錢學森文集(英文版):海外學術文獻(1938~1956)》內容簡介:ThisvolumecollectsthescientiticworksofTsienHsuc-shenaccomplishedduringhisstayintheUnitedStatesasagraduatestudent,scientistandprolessorandpublishedintheperiodof1938~1956,whentheaeronauticexplorationsteppedfromlow-speedtohigh-speedregimesandastronautictechnologyentereditsinfantstage.Inthesepapers,headdressedandsolvedaseriesofkeyproblemsinaerodynamics,stabilityofshells,rocketballisticsandengineanalyses,etc.,someofwhichwerepath-breaking.Startingfrom1946,withhisstrategicwisdom,TsienHsue-shenmadepioneeringcontributionstosomefields,suchasjetpropulsion,engineeringcybernetics,physicalmechanicsandengineeringsciences,andSOon.Alltheseworksfeaturetheuniquemethodologyofturningbasictheoriesinnaturalscienceintopracticaltoolsintacklingcomplicatedengineeringproblems.Itisworthnotingthathefirstadvocatedthephilosophyofengineeringsciences,whichhasbeenelucidatedandillustratedinthevolumeandprovedtobetheguidelineofinnovativeindustrialdevelopment.Thecollectedworksmightbenefittoitsextensivereadersingettingdeeperinsightintotheacademiccontributions,scientificthoughtsandstudyingstyleofTsienfromvariousviewpoints.

目錄

Boundary Layer in Compressible Fluids
Supersonic Flow over an Inclined Body of Revolution
Problems in Motion of Compressible Fluids and Reaction Propulsion
Flight Analvsis of a Sounding Rocket with Special Reference to Propulsion by Successive Impulses
Two-Dimensional Subsonic Flow of Compressible Fluids
The Buckling of Spherical Shells by External Pressure
The Influence of Curvature on the Buckling Characteristics of Structures
A Method for Predicting the Compressibility Burble
The Buckling of Thin Cylindrical Shells under Axial Compression
Buckling of a Column with Non-Linear Lateral Supports
A Theory for the Buckling of Thin Shdls
Heat Conduction across a Partially Insulated Wall
On the Design of the Contraction Cone for a Wind Tunnel
Symmetrical Joukowsky Airfoils in Shear Flow
The“I.imiting I。ine,’in Mixed Subsonic and Supersonic Flow of Compressible Fluids
Loss in Compressor or Turbine due to Twisted Blades
Lifring-Line Theory for a Wing in Non-uniform Flow
Atomic Energy
Two-Dimensional Irrotational Mixed Subsonic and Supersonic Flow of a Compressible Fluid and the Upper Critical Mach Number
Superaerodynamics.Mechanics of Rarefied Gases
Propagation of Plane Sound Waves in Rarefied Gases
Similarity Laws of Hypersonic Flows
One-Dimensional Flows of a Gas Characterized by van der Waals Equation of State
Flow Conditions near the Intersection of a Shock Wave with Sorlid Boundary
Lower Buckling Load in the Non-Linear Buckling Theory for Thin Shells
Rockets and Other Thermal J ets Using Nuclear Energy
Engineering and Engineering Sciences
On Two-Dimensional Non-steady Motion of a Slender Body in a Compressible Fluid
Wind-Tunnel Testing Problems in Superaerodynamics
Airfoils in Slightly Supersonic Flow
Interaction between Parallel Streams of Subsonic and Supersonic Velocities
Research in Rocket and Jet Propulsion
A Generalization Of Alfrey’S Theorem for Visco~elastic Media
Instruction and Research at the Daniel and Florence Guggenheim J et PropulsionCenter
Influence of Flame Front 0n the Flow Field
Optimum Thrust Programming for a Sounding Rocket
The Emission of Radiation from Diatomic Gases.III.Numerical Emissivity Calculations for Carbon Monoxide for Low Optical Densities at 300 K and
Atmospheric Pressure
錢學森生平簡介
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