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包郵 杰弗里·英格拉姆·泰勒科學(xué)論文集:第3卷,空氣動力學(xué)以及落彈數(shù)和爆炸的力學(xué)(英文)
作者：（美）G.K.巴徹勒
開本：
16開
頁數(shù)：
836
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杰弗里·英格拉姆·泰勒科學(xué)論文集:第3卷,空氣動力學(xué)以及落彈數(shù)和爆炸的力學(xué)(英文) 版權(quán)信息
- ISBN：9787560395371
- 條形碼：9787560395371 ; 978-7-5603-9537-1
- 裝幀：一般膠版紙
- 冊數(shù)：暫無
- 重量：暫無
- 所屬分類：>
杰弗里·英格拉姆·泰勒科學(xué)論文集:第3卷,空氣動力學(xué)以及落彈數(shù)和爆炸的力學(xué)(英文) 內(nèi)容簡介
本書是一部版權(quán)引進(jìn)的世界有名科學(xué)家論文集。從1958年到1971年出版的這四卷書中,巴徹勒共收集了杰弗里·英格拉姆·泰勒的近200篇論文前三卷的論文大致按主題分組,第四卷整理了許多有關(guān)流體力學(xué)的論文.這些內(nèi)容加在一起,可以讓讀者徹底了解泰勒爵士在流體動力學(xué)領(lǐng)域的廣泛且多樣的興趣.在第四卷的結(jié)尾,巴徹勒為讀者提供了按時間順序列出的所有四卷論文的清單,以及泰勒爵士發(fā)表的其他文章的清單,從而完成了這項真正寶貴的研究和參考工作。
杰弗里·英格拉姆·泰勒科學(xué)論文集:第3卷,空氣動力學(xué)以及落彈數(shù)和爆炸的力學(xué)(英文) 目錄
1．THE CONDITIONS NECESSARY FOR DISCONTINUOUS MOTION IN GASES．
2．THE USE OF FIN SURFACE TO STABILIZE A WEIGHT TOWED FROM AN AEROPLANE。
3．PRESSURE DISTRIBUTION ROUND A CYLINDER．
4．PRESSURE DISTRIBUTION OVER THE WING OF AN AERO— PLANE IN FLIGHT．
5．ON THE SHAPES OF PARACHUTES．
6．SCIENTIFIC METHODS IN AERONAUTICS．
7．THE ROTATIONAL INFLOW FACTOR IN PROPELLER THEORY．
8．NOTES ON MR GLAUERT’S PAPER，AN AERODYNAMIC THEORY OF THE AIRSCREW．
9．THE SINGING OF WIRES IN A WIND．
10．NOTE ON THE CONNECTION BETWEEN THE LIFT ON AN AEROFOIL IN A WIND AND THE CIRCULATION ROUND IT．
11．A MANOMETER FOR USE WITH SMALL PITOT TUBES．
12．THE ENERGY OF A B0nY MOVING IN AN INFINITE FLUID，WITH AN APPLICATION TO、AIRSHIPS．
13．TⅡE FORCES ON A BODY PLACED IN A CURVED OR CON-VERGING STREAM OF FLUID．
14．A MECHANICAL METHOD FOR SOLVING PROBLEMS OF FLOW IN COMPRESSIBLE FLUIDS(with C．F．Sharman)．
15．THE FLOW OF AIR AT HIGH SPEEDS PAST CURVED SURFACES．
16．SOME CASES OF FLOW OF COMPRESSIBLE FLUIDS．
17．RECENT WORK ON THE FLOW OF COMPRESSIBLE FLUID S．
18．APPLICATIONS TO AERONAUTICS OF ACKERET’S THEORY OF AEROFOILS MOVING AT SPEEDS GREATER THAN THAT OF SOUND．
19．THE AIR PRESSURE ON A CONE MOVING AT HIGH SPEEDS．(with J．W．Maccoll)．
20．THE AIR PRESSURE ON A CONE MOVING AT HIGH SPEEDS．(with J．W．Maccoll)．
21．THE DETERMINATION OF DRAG BY THE PITOT TRAVERSE METHOD．
22．DETERMINATION OF THE PRESSURE INSIDE A HOLLOW BODY IN WHICH THERE ARE A NUMBER OF HOLES COMMUNICATING WITH VARIABLE PRESSURES OUTSIDE．
23．THE PROPAGATION AND D~,CAY OF BLAST WAVES
24．NOTES ON POSSIBLE EQUIPMENT AND TECHNIQUE FOR EXPERIMENT8 ON ICING ON AIRCRAFT
25．GENERATION OF RIPPLES BY WIND BLOWING OVER A VISCOUS FLUID．
26．NOTES ON THE DYNAMICS OF SHOCK-WAVES FROM BARE EXPLOSIVE CHARGES．
27．PRESSURES ON SOLID BODIES NEAR AN EXPLOSION．
28．THE STAGNATION TEMPERATuRE IN A WAKE．
29．THE PROPAGATION OF BLAST WAVES OVER THE GROUND．
30．ANALYSIS OF THE EXPLOSION OF A LONO CYLINDRICAL BOMB DETONATED AT ONE END．
31．TⅡE PRESSURE AND IMPULSE OF SUBMARINE EXPLOSION WAVES ON PLATES．
32．THE DISPERSION OF JETS OF METALS OF Low MELTING POINT IN WATER．
33．THE MOTION OF A BODY IN WATER WHEN SUBJECTED TO A SUDDEN IMPULSE．
34．NOTE ON THE LATEAL EXPANSION BEHIND A DETONATION WAVE(WITH H．Jones)．
35．THE EFFECT OF THE METHOD OF SUPPORT IN TESTS OF DAMAGE TO THIN-WALLED STRUCTURES BY UNDERWATER EXPLOSIONS fwith R．M．Davies)．
36．THE VERTICAL MOTION OF A SPHERICAL BUBBLE AND THEPRESSURE SURROUNDING IT．
37．THE MOTION AND SHAPE OF THE HOLLOW PRODUCED BY ANEXPLOSION IN A LIQUID (with R．M．Daes)．
38．EXPERIMENTS WITH 1/76 SCALE MODEL OF EXPLOSIONS NEAR1/2一SCALE ASSET TARGET(with R．M．Daes)．
39．A FORMULATION OF MRTUCK’S CONCEPTION OF MUNROEJETS．
40．BLAST IMPULSE AND FRAGMENT VELOCITIES FROM CASED CHARGES (with H．Jones)．
41．NOTE ON THE LIMITING RANGES OF LARGE ROCKETS．
42．THE BURSTING OF CYLINDRICAL CASED CHARGES (with H．Jones)．
43．AIR RESISTANCE OF A FLAT PLATE OF VERY POROU, MATERIAL．
44．THE FRAGMENTATION TUBULAR BOMBS．
45．THE AERODYNAMICS OF POROUS SHEETS(with R．M．Davies}．
46．PITOT PRESSURES IN MOIST AIR．
47．THE AIR WAVE SURROUNDING AN EXPANDING SPHERE．
48．THE MECHANICS OF SWIRL ATOMISERS．
49．THE EFFECT OF WIRE GAUZE ON SMALL DISTURBANCES IN A UNIFORM STREAM(with G．K．Batchelor)．
50．THE SHAPE AND ACCELERATION OF A DROP IN A HIGH．SPEED AIR STREAM．
51．THE DYNAMICS OF THE COMBUSTION PRODUCTS BEHIND PLANE AND SPHERICAL DETONATION FRONTS IN EXPLOSIVES．
52．THE MECHANICS OF LARGE BUBBLES RISING THROUGH EXTENDED LIQUIDS AND THROUGH LIQUIDS IN TUBES．
53．THE FORMATION OF A BLAST WAVE FROM A VERY INTENSE EXPLOSION．Ⅰ．THEORETICAL DISCUSSION．
54．THE FORMATION OF A BLAST WAVE BY A VERY INTENSE EXPLOSION．Ⅱ．THE ATOMIC EXPLOSION 0F 1945．
55．THE BOUNDARY LAYER IN THE CONVERGING NOZZLE OF A SWIRL ATOMISER．
56．THE IN8TABILITY OF LIQUID SURFACES WHEN ACCELERATE IN A
2．THE USE OF FIN SURFACE TO STABILIZE A WEIGHT TOWED FROM AN AEROPLANE。
3．PRESSURE DISTRIBUTION ROUND A CYLINDER．
4．PRESSURE DISTRIBUTION OVER THE WING OF AN AERO— PLANE IN FLIGHT．
5．ON THE SHAPES OF PARACHUTES．
6．SCIENTIFIC METHODS IN AERONAUTICS．
7．THE ROTATIONAL INFLOW FACTOR IN PROPELLER THEORY．
8．NOTES ON MR GLAUERT’S PAPER，AN AERODYNAMIC THEORY OF THE AIRSCREW．
9．THE SINGING OF WIRES IN A WIND．
10．NOTE ON THE CONNECTION BETWEEN THE LIFT ON AN AEROFOIL IN A WIND AND THE CIRCULATION ROUND IT．
11．A MANOMETER FOR USE WITH SMALL PITOT TUBES．
12．THE ENERGY OF A B0nY MOVING IN AN INFINITE FLUID，WITH AN APPLICATION TO、AIRSHIPS．
13．TⅡE FORCES ON A BODY PLACED IN A CURVED OR CON-VERGING STREAM OF FLUID．
14．A MECHANICAL METHOD FOR SOLVING PROBLEMS OF FLOW IN COMPRESSIBLE FLUIDS(with C．F．Sharman)．
15．THE FLOW OF AIR AT HIGH SPEEDS PAST CURVED SURFACES．
16．SOME CASES OF FLOW OF COMPRESSIBLE FLUIDS．
17．RECENT WORK ON THE FLOW OF COMPRESSIBLE FLUID S．
18．APPLICATIONS TO AERONAUTICS OF ACKERET’S THEORY OF AEROFOILS MOVING AT SPEEDS GREATER THAN THAT OF SOUND．
19．THE AIR PRESSURE ON A CONE MOVING AT HIGH SPEEDS．(with J．W．Maccoll)．
20．THE AIR PRESSURE ON A CONE MOVING AT HIGH SPEEDS．(with J．W．Maccoll)．
21．THE DETERMINATION OF DRAG BY THE PITOT TRAVERSE METHOD．
22．DETERMINATION OF THE PRESSURE INSIDE A HOLLOW BODY IN WHICH THERE ARE A NUMBER OF HOLES COMMUNICATING WITH VARIABLE PRESSURES OUTSIDE．
23．THE PROPAGATION AND D~,CAY OF BLAST WAVES
24．NOTES ON POSSIBLE EQUIPMENT AND TECHNIQUE FOR EXPERIMENT8 ON ICING ON AIRCRAFT
25．GENERATION OF RIPPLES BY WIND BLOWING OVER A VISCOUS FLUID．
26．NOTES ON THE DYNAMICS OF SHOCK-WAVES FROM BARE EXPLOSIVE CHARGES．
27．PRESSURES ON SOLID BODIES NEAR AN EXPLOSION．
28．THE STAGNATION TEMPERATuRE IN A WAKE．
29．THE PROPAGATION OF BLAST WAVES OVER THE GROUND．
30．ANALYSIS OF THE EXPLOSION OF A LONO CYLINDRICAL BOMB DETONATED AT ONE END．
31．TⅡE PRESSURE AND IMPULSE OF SUBMARINE EXPLOSION WAVES ON PLATES．
32．THE DISPERSION OF JETS OF METALS OF Low MELTING POINT IN WATER．
33．THE MOTION OF A BODY IN WATER WHEN SUBJECTED TO A SUDDEN IMPULSE．
34．NOTE ON THE LATEAL EXPANSION BEHIND A DETONATION WAVE(WITH H．Jones)．
35．THE EFFECT OF THE METHOD OF SUPPORT IN TESTS OF DAMAGE TO THIN-WALLED STRUCTURES BY UNDERWATER EXPLOSIONS fwith R．M．Davies)．
36．THE VERTICAL MOTION OF A SPHERICAL BUBBLE AND THEPRESSURE SURROUNDING IT．
37．THE MOTION AND SHAPE OF THE HOLLOW PRODUCED BY ANEXPLOSION IN A LIQUID (with R．M．Daes)．
38．EXPERIMENTS WITH 1/76 SCALE MODEL OF EXPLOSIONS NEAR1/2一SCALE ASSET TARGET(with R．M．Daes)．
39．A FORMULATION OF MRTUCK’S CONCEPTION OF MUNROEJETS．
40．BLAST IMPULSE AND FRAGMENT VELOCITIES FROM CASED CHARGES (with H．Jones)．
41．NOTE ON THE LIMITING RANGES OF LARGE ROCKETS．
42．THE BURSTING OF CYLINDRICAL CASED CHARGES (with H．Jones)．
43．AIR RESISTANCE OF A FLAT PLATE OF VERY POROU, MATERIAL．
44．THE FRAGMENTATION TUBULAR BOMBS．
45．THE AERODYNAMICS OF POROUS SHEETS(with R．M．Davies}．
46．PITOT PRESSURES IN MOIST AIR．
47．THE AIR WAVE SURROUNDING AN EXPANDING SPHERE．
48．THE MECHANICS OF SWIRL ATOMISERS．
49．THE EFFECT OF WIRE GAUZE ON SMALL DISTURBANCES IN A UNIFORM STREAM(with G．K．Batchelor)．
50．THE SHAPE AND ACCELERATION OF A DROP IN A HIGH．SPEED AIR STREAM．
51．THE DYNAMICS OF THE COMBUSTION PRODUCTS BEHIND PLANE AND SPHERICAL DETONATION FRONTS IN EXPLOSIVES．
52．THE MECHANICS OF LARGE BUBBLES RISING THROUGH EXTENDED LIQUIDS AND THROUGH LIQUIDS IN TUBES．
53．THE FORMATION OF A BLAST WAVE FROM A VERY INTENSE EXPLOSION．Ⅰ．THEORETICAL DISCUSSION．
54．THE FORMATION OF A BLAST WAVE BY A VERY INTENSE EXPLOSION．Ⅱ．THE ATOMIC EXPLOSION 0F 1945．
55．THE BOUNDARY LAYER IN THE CONVERGING NOZZLE OF A SWIRL ATOMISER．
56．THE IN8TABILITY OF LIQUID SURFACES WHEN ACCELERATE IN A
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