| Numbering |
Thesis Name |
Joint Author |
| FM04-003 |
Flowfield prediction of a probe entering the Martian atmosphere |
Junming Lu, Qiang Wang, Xiaoli Cheng |
| FM04-004 |
Early-time interface instabilities in high intensity aero-breakup of liquid drop |
Xiangyu Hu, Nikolaus A. Adams |
| FM04-005 |
Compressible fluid-structure interaction simulations of an
inflatable tension cone decelerator for planetary re-entry |
Carlos Pantano, Richard Kramer, Fehmi Cirak |
| FM04-006 |
Ring-pattern formation in the rotating stellar structures |
Sugimoto Takeshi |
| FM04-007 |
On the linearity of the quieting of high speed jets by heating |
Daniel J. Bodony |
| FM04-009 |
Supersonic flow structure on compression surfaces of model inlet
under plasma impact |
Sergey Leonov, Alexander Firsov, Dmitry Yarantsev, Marat Goldfeld, Konstantin Timofeev, Francois Falempin |
| FM04-010 |
Investigations of supersonic flow past micro ramp and vanes |
Dawen Xue, Zhihua Chen, Xiaohui Sun, Yaohui Chen |
| FM04-011 |
Aerothermal Optimization of Hypersonic Vehicle Leading Edge Based on Genetic Algorithm |
Cui K., Hu S.C., Gao T.Y., Wang X.P., Yang G.W. |
| FM04-012 |
Numerical simulation shock wave buffet on an OAT15A airfoil by IDDES hybrid methods |
Jingbo Huang, Zhixiang Xiao, Jian Liu, Song Fu |
| FM04-013 |
A multi-layer model for mean velocity and density profile in
compressible channel flow |
Yanzhi Wang, Zhensu She, Fazle Hussain |
| FM04-014 |
Quantifying Mach number similarity of compressible turbulent boundary |
Yousheng Zhang, Weitao Bi, Zhensu She, Fazle Hussain |
| FM04-015 |
On the evolution of a heavy-gas cylinder accelerated by a cylindrical converging shock wave: effect of initial conditions |
Ting Si, Zhigang Zhai, Xisheng Luo, Jiming Yang |
| FM04-016 |
Analysis of an aero-acoustic flow field using dynamic modes |
Peter J. Schmid, Xavier Garnaud, Lutz Lesshafft, Patrick Huerre |
| FM04-017 |
Analysis of continuous adjoint control of compressible plane jets |
Daniel Marinc, Holger Foysi |
| FM04-018 |
Development of the $\varGamma-Re_\varTheta_t$ transition model for high speed flows |
Yancheng You |
| FM04-019 |
A new method for measuring specific heat ratio of combustion gases in hypersonic flow |
Tiejin Wang, Jun Chen |
| FM04-020 |
Visualization experimental and numerical investigation on the muzzle flow |
Zeqing Guo, Xiaohai Jiang, Yang Wang, Zhihua Chen, Hongzhi Li |
| FM04-021 |
A numerical investigation of injection angle effect on lateral jet
interaction for revolution body |
Yuwei Liu, Zhaoyong Ni, Yaofeng Liu |
| FM04-022 |
Experimental study on vortex/bow shock interaction at Mach number of 6 |
Andrey Shmakov, Andrey Shevchenko, Anatoly Kharitonov |
| FM04-023 |
Nonlinear stability of the supersonic boundary layer under the
consideration of receptivity to slow acoustic waves |
Yihong Fang, Cuiping Li, Yifang Liu |
| FM04-024 |
Characterization of turbulent transition and shock/boundary-layer interaction in shock tubes |
Yong Sun, Matthias Ihme, Ralf Deiterding |
| FM04-025 |
Inviscid quasistatic modelling for unsteady shock reflections with separation |
Lionel Agostini, Lionel Larcheveque, Pierre Dupont |
| FM04-026 |
Disturbance evolution in a Mach 4.8 boundary layer with separation |
Olaf Marxen, Thierry Magin, Gianluca Iaccarino |
| FM04-028 |
Elementary waves of riemann problem and Interaction with a weak discontinuity |
Radha R., Sharma V.D. |
| FM04-029 |
Physical analysis of compressibility effects in the transonic flow
around a supercritical airfoil at high reynolds number by
numerical simulation |
Damien Szubert, Fernando Grossi, Marianna Braza, Yannick Hoarau, Gilles Harran, Alain Sevrain |
| FM04-030 |
Effect of thermal actuators on drag reduction in a Mach 8 bow shock |
Hong Yan, Xiaojing Yu, Jijun Yu |
| |
|
|
