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Home > Shock Waves: Proceedings of the 24th International Symposium on Shock Waves, Beijing, China, July 11-16 2004, Vol. 1 and 2 > Massively parallel computation of three-dimensional scramjet combustor
Shock Waves: Proceedings of the 24th International Symposium on Shock Waves, Beijing, China, July 11-16 2004, Vol. 1 and 2 |
Zonglin Jiang
Springer Berlin Heidelberg
Shock Waves: Proceedings of the 24th International Symposium on Shock Waves, Beijing, China, July 11-16 2004, Vol. 1 and 2
Massively parallel computation of three-dimensional scramjet combustor
Authors

Z. H. Zheng; J. L. Le

ARI Id

1664279167226_1040662

Access

Not Available Free

Pages

897-902

DOI

10.1007/978-3-540-27009-6_136

Chapter URL

https://rd.springer.com/chapter/10.1007/978-3-540-27009-6_136

Table of Contents of Book
Showing 1 to 20 of 222 entries
Chapters/HeadingsAuthor(s)PagesInfo
Front Matter
I-XXII
Front Matter
1-1
Summary of forty years continuous shock wave research at interdisciplinary shock wave research center, Tohoku University
K. Takayama
3-10
Precursor kinetics and nanoparticle synthesis studied in a shock wave reactor
P. Roth; A. Giesen
11-18
The propagation mechanism of cellular detonation
J. H. S. Lee
19-30
The development of the HyShot flight program
A. Paull; H. Alesi; S. Anderson
31-48
Shock induced porous barrier flows, with underlying wall pressure amplification
B. W. Skews; S. Bugarin
49-56
The single pulse shock tube: its Odyssey in chemical kinetics
A. Lifshitz
57-64
Recent developments with gaseous detonation drivers for a shock tunnel
H-r Yu
65-73
Some perspectives on pulse detonation propulsion systems
F. K. Lu; D. R. Wilson
75-86
Front Matter
87-87
Laser energy deposition in Edney IV interaction
D. Knight; R. Adelgren; G. Elliott; H. Yan; T. Beutner
89-94
Hypersonic wave drag reduction in re-entry capsules using concentrated energy deposition
K. Satheesh; G. Jagadeesh; P. S. Kulkarni
95-100
Supersonic flow over double cone geometries
H. Kleine; K. Hiraki
101-106
An expansion tube study of high enthalpy carbon-dioxide flows
T. J. Mclntyre; T. N. Eichmann; I. Lourel; K. M. Hajek; H. Rubinsztein-Dunlop
107-112
Shock tunnel measurement of the interaction amplification factor for a hot gas side jet in a supersonic cross flow
M. Havermann; H. Ende; F. Seiler; M. Schwenzer
113-118
Drag reduction by controlled base flow separation for missile shaped bodies flying at hypersonic Mach number
V. Menezes; M. Sun; G. Jagadeesh; K. P. J. Reddy; K. Takayama
119-124
Improvement of aerospike nozzle efficiency due to change of plug base configuration
S. Aso; K. Sugimoto
125-130
Measurement and calculation of vibrational temperature behind strong shock waves
R. L. Zhang; J. L. Le; J. P. Cui; F. M. Yu; L. H. Han; S. Wang et al.
131-136
Interference effects due to a transverse slot jet in a hypersonic flow
F. C. Dixon; G. T. Roberts; O. R. Tutty
137-142
Chapters/HeadingsAuthor(s)PagesInfo
Showing 1 to 20 of 222 entries
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