Hannemann, Klaus
Shock Waves
Part I. Plenary Lectures
1. Relaxation effects in hypervelocity flow: selected contributions from the T5 Lab
H.G. Hornung
2. CFD contributions to high-speed shock-related problems
K. Fujii
3. Explosive eruptions of volcanos: simulation shock tube methods and multi-phase mathematical models
V. Kedrinskiy
4. Ignition delay time measurements at practical conditions using a shock tube
E.L. Petersen
5. Material processing and surface reaction studies in free piston driven shock tube
K.P.J. Reddy, M.S. Hegde, V. Jayaram
6. Molecular dynamics of shock waves in dense fluids
S. Schlamp, B.C. Hathorn
7. SBLI control for wings and inlets
H. Babinsky, H. Ogawa
8. Shock pattern in the plume of rocket nozzles - needs for design consideration
G. Hagemann
Part II. Blast Waves
9. A quick estimate of explosion-induced stress field in various media
A. Sakurai, K. Tanaka
10. Attenuation properties of blast wave through porous layer
K. Kitagawa, S. Yamashita, K. Takayama, M. Yasuhara
11. Blast wave reflection from lightly destructible wall
V.V. Golub, T.V. Bazhenova, O.A. Mirova, Y.L. Sharov, V.V. Volodin
12. Gram-range explosive blast scaling and associated materials response
M.J. Hargather, G.S. Settles, J.A. Gatto
13. High-speed digital shadowgraphy of shock waves from explosions and gunshots
M.M. Biss, G.S. Settles, M.J. Hargather, L.J. Dodson, J.D. Miller
14. Modelling high explosives (HE) using smoothed particle hydrodynamics
M. Omang, S. Børve, J. Trulsen
15. Modification of air blast loading transmission by foams and high density materials
B.E. Gelfand, M.V. Silnikov, M.V. Chernyshov
16. Multifunctional protective devices for localizing the blast impact when conducting the ground and underwater operations of explosion cutting
B.I. Palamarchuk, A.T. Malakhov, A.N. Manchenko, A.V. Cherkashin, N.V. Korpan
17. Propagation of the shock wave generated by two-dimensional beam focusing of a CO
S. Udagawa, Y. Yamamoto, S. Nakajima, K. Takei, K. Ohmura, K. Maeno
18. Simulation of strong blast waves by simultaneous detonation of small charges - a conceptual study
A. Klomfass, G. Heilig, H. Klein
19. Small-scale installation for research of blast wave dynamics
N.P. Mende, A.B. Podlaskin, A.M. Studenkov
20. Strong blast in a heterogeneous medium
B.I. Palamarchuk
Part III. Chemically Reacting Flows
21. Atomized fuel combustion in the reflected-shock region
B. Rotavera, E.L. Petersen
22. Coupling CFD and chemical kinetics: examples Fire II and TITAN aerocapture
P. Leyland, S. Heyne, J.B. Vos
23. Experimental investigation of catalytic and non-catalytic surface reactions on
V. Jayaram, G.M. Hegde, M.S. Hegde, K.P.J. Reddy
24. Experimental investigation of interaction of strong shock heated oxygen gas on the surface of ZrO
V. Jayaram, M.S. Hegde, K.P.J. Reddy
25. Further studies on initial stages in the shock initiated H
K. Yasunaga, D. Takigawa, H. Yamada, T. Koike, Y. Hidaka
26. Shock-tube development for high-pressure and low-temperature chemical kinetics experiments
J. Vries, C. Aul, A. Barrett, D. Lambe, E. Petersen
27. Shock-tube study of tert-butyl methyl ether pyrolysis
K. Yasunaga, Y. Hidaka, A. Akitomo, T. Koike
28. Temperature dependence of the soot yield in shock wave pyrolysis of carbon-containing precursors
A. Drakon, A. Emelianov, A. Eremin, A. Makeich, H. Jander, H.G. Wagner, C. Schulz, R. Starke
29. Thermal reactions of o-dichlorobenzene. Single pulse shock tube investigation
A. Lifshitz, A. Suslensky, C. Tamburu
30. Wall heat transfer in shock tubes at long test times
C. Frazier, A. Kassab, E.L. Petersen
Part IV. Detonation and Combustion
31. A study on DDT processes in a narrow channel
K. Nagai, T. Okabe, K. Kim, T. Yoshihashi, T. Obara, S. Ohyagi
32. Combustion in a horizontal channel partially filled with porous media
C. Johansen, G. Ciccarelli
33. Continuum/particle interlocked simulation of gas detonation
A. Kawano, K. Kusano
34. Dependence of PDE performance on divergent nozzle and partial fuel filling
Z.X. Liang, Y.J. Zhu, J.M. Yang
35. Direct Monte-Carlo simulation of developing detonation in gas
Z.A. Walenta, K. Lener
36. Effects of detailed chemical reaction model on detonation simulations
N. Tsuboi, M. Asahara, A.K. Hayashi, M. Koshi
37. Effects of flame jet configurations on detonation initiation
K. Ishii, T. Akiyoshi, M. Gonda, M. Murayama
38. Experimental and theoretical investigation of detonation and shock waves action on phase of hydrocarbon mixture in porous media
D.I. Baklanov, L.B. Director, S.V. Golovastov, V.V. Golub, I.L. Maikov, V.M. Torchinsky, V.V. Volodin, V.M. Zaichenko
39. Experimental and theoretical study of valveless fuel supply system for PDE
D.I. Baklanov, S.V. Golovastov, N.W. Tarusova, L.G. Gvozdeva
40. Experimental investigation of the ignition spark shock waves influence on detonation formation in hydroxygen mixtures
D.I. Baklanov, S.V. Golovastov, V.V. Golub, V.V. Volodin
41. Experimental study on the nonideal detonation for JB-9014 rate sticks
L. Zou, D. Tan, S. Wen, J. Zhao, C. Liu
42. Experimental study on transmission of an overdriven detonation wave across a mixture
J. Li, K. Chung, W.H. Lai, F.K. Lu
43. Flow vorticity behavior in inhomogeneous supersonic flow past shock and detonation waves
V.A. Levin, G.A. Skopina
44. Ground reflection interaction with height-of-burst metalized explosions
R.C. Ripley, L. Donahue, T.E. Dunbar, S.B. Murray, C.J. Anderson, F. Zhang, D.V. Ritzel
45. High-fidelity numerical study on the on-set condition of oblique detonation wave cell structures
J.Y. Choi, E.J.R. Shin, D.R. Cho, I.S. Jeung
46. High-pressure shock tube experiments and modeling of n-dodecane/air ignition
S.S. Vasu, D.F. Davidson, R.K. Hanson
47. Implicit-explicit Runge-Kutta methods for stiff combustion problems
E. Lindblad, D.M. Valiev, B. Müller, J. Rantakokko, P. Lütstedt, M.A. Liberman
48. Near-field blast phenomenology of thermobaric explosions
D.V. Ritzel, R.C. Ripley, S.B. Murray, J. Anderson
49. Numerical and theoretical analysis of the precursor shock wave formation at high-explosive channel detonation
P. Vu, H.W. Leung, V. Tanguay, R. Tahir, E. Timofeev, A. Higgins
50. Numerical study on shockwave structure of superdetonative ram accelerator
K. Sung, I.-S. Jeung, F. Seiler, G. Patz, G. Smeets, J. Srulijes
51. Numerical study on the self-organized regeneration of transverse waves in cylindrical detonation propagations
C. Wang, Z. Jiang
52. On the mechanism of detonation initiations
Z. Jiang, H. Teng, D. Zhang, S.V. Khomik, S.P. Medvedev
53. Overview of the 2005 Northern Lights Trials
S.B. Murray, C.J. Anderson, K.B. Gerrard, T. Smithson, K. Williams, D.V. Ritzel
54. Physics of detonation wave propagation in 3D numerical simulations
H.-S. Dou, B.C. Khoo, H.M. Tsai
55. Propagation of cellular detonation in the plane channels with obstacless
V. Levin, V. Markov, T. Zhuravskaya, S. Osinkin
56. Re-initiation of detonation wave behind slit-plate
J. Sentanuhady, Y. Tsukada, T. Obara, S. Ohyagi
57. Shock-to-detonation transition due to shock interaction with prechamber-jet cloud
S.M. Frolov, V.S. Aksenov, V.Y. Basevich
58. Shock-to-detonation transition in tube coils
S.M. Frolov, I.V. Semenov, I.F. Ahmedyanov, V.V. Markov
59. Simulation of hydrogen detonation following an accidental release in an enclosure
L. Fang, L. Bédard-Tremblay, L. Bauwens, Z. Cheng, A.V. Tchouvelev
60. Spectroscopic studies of micro-explosions
G. Hegde, A. Pathak, G. Jagadeesh, C. Oommen, E. Arunan, K.P.J. Reddy
61. Structural response to detonation loading in 90-degree bend
Z. Liang, T. Curran, J.E. Shepherd
62. Study on perforated plate induced deflagration waves in a smooth tube
Y.J. Zhu, Z.X. Liang, J.H.S. Lee, J.M. Yang
63. Unconfined aluminum particles-air detonation
F. Zhang, K.B. Gerrard, R.C. Ripley, V. Tanguay
64. Viscous attenuation of a detonation wave propagating in a channel
P. Ravindran, R. Bellini, T.-H. Yi, F.K. Lu
Part V. Diagnostics
65. A diode laser absorption sensor for rapid measurements of temperature and water vapor in a shock tube
H. Li, A. Farooq, R.D. Cook, D.F. Davidson, J.B. Jeffries, R.K. Hanson
66. A novel fast-response heat-flux sensor for measuring transition to turbulence in the boundary layer behind a moving shock wave
T. Roediger, H. Knauss, J. Srulijes, F. Seiler, E. Kraemer
67. Application of HEG static pressure probe in HIEST
T. Hashimoto, S. Rowan, T. Komuro, K. Sato, K. Itoh, M. Robinson, J. Martinez Schramm, K. Hannemann
68. Application of laser-induced thermal acoustics to temperature measurement of the air behind shock waves
T. Mizukaki
69. Assessment of rotational and vibrational temperatures behind strong shock waves derived from CARS method
A. Matsuda, M. Ota, K. Arimura, S. Bater, K. Maeno, T. Abe
70. Availability of the imploding technique as an igniter for large-scale natural-gas-engines
T. Tsuboi, S. Nakamura, K. Ishii, M. Suzuki
71. Experimental study of SiC-based ablation products in high-temperature plasma-jets
M. Funatsu, H. Shirai
72. On pressure measurements in blast wave flow fields generated by milligram charges
S. Rahman, E. Timofeev, H. Kleine, K. Takayama
73. Quantitative diagnostics of shock wave - boundary layer interaction by digital speckle photography
N. Fomin, E. Lavinskaya, P. Doerffer, J.-A. Szumski, R. Szwaba, J. Telega
Part VI. Facilities
74. A simulation technique for radiating shock tube flows
R.J. Gollan, C.M. Jacobs, P.A. Jacobs, R.G. Morgan, T.J. McIntyre, M.N. Macrossan, D.R. Buttsworth, T.N. Eichmann, D.F. Potter
75. Aerodynamic force measurement technique with accelerometers in the impulsive facility HIEST
H. Tanno, T. Komuro, K. Sato, K. Itoh
76. On the free-piston shock tunnel at UniBwM (HELM)
K. Schemperg, C. Mundt
77. Progress towards a microfabricated shock tube
G. Mirshekari, M. Brouillette
Part VII. Flow Visualisation
78. A tool for the design of slit and cutoff in schlieren method
D. Kikuchi, M. Anyoji, M. Sun
79. Application of pressure-sensitive paints in high-speed flows
H. Zare-Behtash, N. Gongora, C. Lada, D. Kounadis, K. Kontis
80. Doppler Picture Velocimetry (DPV) applied to hypersonics
A. Pichler, A. George, F. Seiler, J. Srulijes, M. Havermann
81. On the conservation laws for light rays across a shock wave: Toward computer design of an optical setup for flow visualization
M. Sun
82. Shock stand-off distance over spheres flying at transonic speed ranges in air
T. Kikuchi, D. Numata, K. Takayama, M. Sun
83. Shock tube study of the drag coefficient of a sphere
G. Jourdan, L. Houas, O. Igra, J.-L. Estivalezes, C. Devals, E.E. Meshkov
84. Three-dimensional interferometric CT measurement of discharging shock/vortex flow around a cylindrical solid body
M. Ota, T. Inage, K. Maeno
85. Vizualization of 3D non-stationary flow in shock tube using nanosecond volume discharge
I.A. Znamenskaya, I.V. Mursenkova, T.A. Kuli-Zade, A.N. Kolycheva
Part VIII. Hypersonic Flow
86. Assessment of the convective and radiative transfers to the surface of an orbiter entering a Mars-like atmosphere
N. Bédon, M.-C. Druguet, D. Zeitoun, P. Boubert
87. Base pressure and heat transfer on planetary entry type configurations
G. Park, S. L. Gai, A. J. Neely, R. Hruschka
88. Combustion performance of a scramjet engine with inlet injection
S. Rowan, T. Komuro, K. Sato, K. Itoh
89. COMPARE, a combined sensor system for re-entry missions
A. Preci, G. Herdrich, M. Gräßlin, H.-P. Röser, M. Auweter-Kurtz
90. Drag reduction by a forward facing aerospike for a large angle blunt cone in high enthalpy flows
V. Kulkarni, P.S. Kulkarni, K.P.J. Reddy
91. Drag reduction by counterflow supersonic jet for a blunt cone in high enthalpy flows
V. Kulkarni, K.P.J. Reddy
92. Effect of electric arc discharge on hypersonic blunt body drag
K. Satheesh, G. Jagadeesh
93. Effect of the nose bluntness on the electromagnetic flow control for reentry vehicles
H. Otsu, T. Matsumura, Y. Yamagiwa, M. Kawamura, H. Katsurayama, A. Matsuda, T. Abe, D. Konigorski
94. Enhanced design of a scramjet intake using two different RANS solvers
M. Krause, J. Ballmann
95. Experimental and numerical investigation of film cooling in hypersonic flows
K.A. Heufer, H. Olivier
96. Experimental and numerical investigation of jet injection in a wall bounded supersonic flow
J. Ratan, G. Jagadeesh
97. Experimental investigation of cowl shape and location on inlet characteristics at hypersonic Mach number
D. Mahapatra, G. Jagadeesh
98. Experimental investigation of heat transfer reduction using forward facing cavity for missile shaped bodies flying at hypersonic speed
S. Saravanan, K. Nagashetty, G. Jagadeesh, K.P.J. Reddy
99. Extrapolation of a generic scramjet model to flight scale by experiments, flight data and CFD
A. Mack, J. Steelant, K. Hannemann
100. Force measurements of blunt cone models in the HIEST high enthalpy shock tunnel
K. Sato, T. Komuro, M. Takahashi, T. Hashimoto, H. Tanno, K. Itoh
101. Investigations of separated flow over backward facing steps in IISc hypersonic shock tunnel
P. Reddeppa, K. Nagashetty, G. Jagadeesh
102. Measurement of aerodynamic forces for missile shaped body in hypersonic shock tunnel using 6-component accelerometer based balance system
S. Saravanan, G. Jagadeesh, K.P.J. Reddy
103. Measurement of shock stand-off distance on a 120° blunt cone model at hypersonic Mach number in Argon
K. Satheesh, G. Jagadeesh
104. Model for shock interaction with sharp area reduction
J. Falcovitz, O. Igra
105. Modelling dissociation in hypersonic blunt body and nozzle flows in thermochemical nonequilibrium
E. Josyula, W.F. Bailey
106. Numerical and experimental investigation of viscous shock layer receptivity and instability
A. Kudryavtsev, S. Mironov, T. Poplavskaya, I. Tsyryulnikov
107. Numerical rebuilding of the flow in a valve-controlled Ludwieg tube
T. Wolf, M. Estorf, R. Radespiel
108. Numerical study of shock interactions in viscous, hypersonic flows over double-wedge geometries
Z.M. Hu, R.S. Myong, T.H. Cho
109. Numerical study of thermochemical relaxation phenomena in high-temperature nonequilibrium flows
S. Kumar, H. Olivier, J. Ballmann
110. Numerical study of wall temperature and entropy layer effects on transitional double wedge shock wave/boundary layer interactions
T. Neuenhahn, H. Olivier
111. Similarity laws of re-entry aerodynamics - analysis of reverse flow shock and wake flow thermal inversion phenomena
S. Balage, R. Boyce, N. Mudford, H. Ranadive, S. Gai
112. Simultanous measurements of 2-D total radiation and CARS data from hypervelocity flow behind strong shock waves
K. Maeno, M. Ota, A. Matsuda, B. Suhe, K. Arimura
113. Shock tunnel testing of a Mach 6 hypersonic waverider
K. Hemanth, G. Jagadeesh, S. Saravanan, K. Nagashetty, K.P.J. Reddy
114. Supersonic flow over axisymmetric cavities
Khadijeh Mohri, Richard Hillier
115. Tandem spheres in hypersonic flow
S.J. Laurence, R. Deiterding, H.G. Hornung
116. Three dimensional experimental investigation of a hypersonic double-ramp flow
F.F.J. Schrijer, R. Caljouw, F. Scarano, B.W. Oudheusden
117. Triple point shear layers in hypervelocity flow
M. Sharma, L. Massa, J.M. Austin
Part IX. Ignition
118. Auto-ignition of hydrogen-air mixture at elevated pressures
A.N. Derevyago, O.G. Penyazkov, K.A. Ragotner, K.L. Sevruk
119. Discrepancies between shock tube and rapid compression machine ignition at low temperatures and high pressures
E.L. Petersen, M. Lamnaouer, J. Vries, H. Curran, J. Simmie, M. Fikri, C. Schulz, G. Bourque
120. Ignition delay studies on hydrocarbon fuel with and without additives
M. Nagaboopathy, G. Hegde, K.P.J. Reddy, C. Vijayanand, M. Agarwal, D.S.S. Hembram, D. Bilehal, E. Arunan
121. Ignition of hydrocarbon–containing mixtures by nanosecond discharge: experiment and numerical modelling
I.N. Kosarev, S.V. Kindusheva, N.L. Aleksandrov, S.M. Starikovskaia, A.Y. Starikovskii
122. Laser-based ignition of hydrogen-oxygen mixture
Y.V. Tunik, O. Haidn, O.P. Shatalov
123. Measurements of ignition delay times and OH species concentrations in DME/O
R.D. Cook, D.F. Davidson, R.K. Hanson
124. Shock tube study of artificial ignition of N
I.N. Kosarev, S.M. Starikovskaia, A.Y. Starikovskii
125. Shock tube study of kerosene ignition delay
S. Wang, B.C. Fan, Y.Z. He, J.P. Cui
126. Shock-tube study of the ignition delay time of tetraethoxysilane (TEOS)
A. Abdali, M. Fikri, H. Wiggers, C. Schulz
Nyckelord: Engineering, Engineering Thermodynamics, Heat and Mass Transfer, Mechanics, Fluids, Thermodynamics, Engineering Fluid Dynamics, Fluids, Acoustics, Automotive Engineering
- Författare
- Hannemann, Klaus
- Seiler, Friedrich
- Utgivare
- Springer
- Utgivningsår
- 2009
- Språk
- en
- Utgåva
- 1
- Sidantal
- 829 sidor
- Kategori
- Teknologi, energi, trafik
- Format
- E-bok
- eISBN (PDF)
- 9783540851684