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                             32 gevonden resultaten
nr titel auteur tijdschrift jaar jaarg. afl. pagina('s) type
1 Adaptive Cartesian cut-cell sharp interface method (aC3SIM) for three-dimensional multi-phase flows Kim, H.

8 p. 1023-1041
artikel
2 Aerodynamic design of integrated propulsion–airframe configuration of a hybrid wing body aircraft Liou, M.-F.

8 p. 1043-1064
artikel
3 An adaptive discontinuity fitting technique on unstructured dynamic grids Chang, S.

8 p. 1103-1115
artikel
4 An improvement of the AUSMDV+ scheme on unstructured grids Phongthanapanich, S.

8 p. 901-927
artikel
5 A simplified burn model for simulating explosive effects and afterburning Houim, R. W.

8 p. 851-875
artikel
6 AUSM scheme: its application to a realistic combustor configuration, the Energy Efficient Engine Miki, K.

8 p. 1009-1021
artikel
7 Beirut explosion: TNT equivalence from the fireball evolution in the first 170 milliseconds Aouad, C. J.

8 p. 813-827
artikel
8 Characterization of blast waves using solid and gaseous explosives: application to dynamic buckling of cylindrical shells Thierry, V.

8 p. 703-713
artikel
9 Computation of shock wave structure using a simpler set of generalized hydrodynamic equations based on nonlinear coupled constitutive relations Jiang, Z.

8 p. 1227-1239
artikel
10 Continuous multifront detonation of kerosene–air mixture in an annular combustor with variations of its geometry Bykovskii, F. A.

8 p. 829-839
artikel
11 Correction to: Modelling of Mach reflections in internal axisymmetric steady supersonic flow Shoesmith, B.

8 p. 959-960
artikel
12 Development of a steady detonation reactor with state-to-state thermochemical modeling Vargas, J.

8 p. 679-689
artikel
13 Free-standing conical shock Mölder, S.

8 p. 753-758
artikel
14 Gap-induced transition via oblique breakdown at Mach 6 Xue, Y.

8 p. 1181-1190
artikel
15 Improved shock-reloading technique for dynamic yield strength measurements Li, X.

8 p. 727-732
artikel
16 Large eddy simulation of acoustic waves generated from a hot supersonic jet Nonomura, T.

8 p. 1133-1154
artikel
17 Limitation principle for computational fluid dynamics Liu, C.

8 p. 1083-1102
artikel
18 Modelling of Mach reflections in internal axisymmetric steady supersonic flow Shoesmith, B.

8 p. 945-957
artikel
19 Nonlinear subscale turbulent models for very large eddy simulation of turbulent flows Shih, T.-H.

8 p. 1155-1179
artikel
20 Numerical investigation of the liquid-fueled pulse detonation engine for different operating conditions Nguyen, V. B.

8 p. 1205-1225
artikel
21 Numerical study on the shock transitions during off-design operation of a dual throat thruster Jayakrishnan, S.

8 p. 929-943
artikel
22 Resonance and mode locking in gaseous detonation propagation in a periodically nonuniform medium Kasimov, A. R.

8 p. 841-849
artikel
23 Second memorial issue in honor of Dr. Meng-Sing Liou Chang, C.-H.

8 p. 1007-1008
artikel
24 Shock ignition of aluminium particle clouds in the low-temperature regime Omang, M.

8 p. 691-701
artikel
25 Shock wave response of porous carbon fiber–epoxy composite Mochalova, V.

8 p. 715-725
artikel
26 Skew-symmetric splitting of high-order central schemes with nonlinear filters for computational aeroacoustics turbulence with shocks Sjögreen, B.

8 p. 1117-1132
artikel
27 Spatial and spectral structure of explosively generated plasmas in tubes Poirier, N.

8 p. 877-886
artikel
28 The effect of increasing rarefaction on the formation of Edney shock interaction patterns: type-I to type-VI Agir, M. B.

8 p. 733-751
artikel
29 The effects of electrically exploding gold bridgewires into inert and explosive powder beds Rae, P. J.

8 p. 887-900
artikel
30 The HLLC Riemann solver Toro, E. F.

8 p. 1065-1082
artikel
31 Thermo-chemical analyses of steady detonation wave using the Shock and Detonation Toolbox in Cantera Li, Z.

8 p. 759-762
artikel
32 Uncertainty quantification of shock–bubble interaction simulations Jin, J.

8 p. 1191-1204
artikel
                             32 gevonden resultaten
 
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