All Stories

  1. Flow control strategy for stably generating vortex
  2. Extraction of Speed-Control Strategy in En-Route Air Traffic using Multi-Objective Optimization and Decision Tree
  3. Feature extraction of fields of fluid dynamics data using sparse convolutional autoencoder
  4. A high-fidelity body-force modeling approach for plasma-based flow control simulations
  5. Flow-Control Experiment around Half-Span Wing Model for DBD-PA Application on UAV
  6. Flight Test of UAV with DBD-Pa Flow Control
  7. Mechanism of flow separation control with DBD plasma actuator obtained by Ape X Deep Q Network Control
  8. Multi-Objective Takeoff Time Optimization Using Cellular Automaton-Based Simulator
  9. Computational Study of Wing-Tip Effect for Flow-Control Authority of Dielectric-Barrier-Discharge Plasma Actuator
  10. Closed-Loop Flow Separation Control Using the Deep Q Network over Airfoil
  11. Flow-control capability of electronic-substrate-sized power supply for a plasma actuator
  12. Separated Flow Control of Small Horizontal-Axis Wind Turbine Blades Using Dielectric Barrier Discharge Plasma Actuators
  13. Flow Control on an Unmanned Aerial Vehicle Using a Plasma Actuator Driven By a Substrate-Size Power Supply
  14. Aerodynamics of Owl-like Wing Model at Low Reynolds Numbers
  15. Mechanisms for turbulent separation control using plasma actuator at Reynolds number of 1.6 × 106
  16. Computational Study of Wing Tip Effect for the Flow Control Authority of DBD Plasma Actuator
  17. Preliminary Study of Multi-Objective Air Traffic Optimization by Using Step Back Cellular Automaton
  18. Large eddy simulation of acoustic waves generated from a hot supersonic jet
  19. Aerodynamic drag reduction of a simplified vehicle model by promoting flow separation using plasma actuator
  20. Dominant parameters for maximum velocity induced by body-force models for plasma actuators
  21. Three Flow Features behind the Flow Control Authority of DBD Plasma Actuator: Result of High-Fidelity Simulations and the Related Experiments
  22. Identification of Acoustic Wave Propagation Pattern of a Supersonic Jet Using Frequency-Domain POD
  23. Effect of Mach Number on Airfoil Characteristics at Reynolds Number of 3,000
  24. Preliminary Study of Multi-Objective Air Traffic Optimization by using Step Back Cellular Automaton
  25. Aerodynamic drag reduction by controlling flow structure of simplified vehicle model using plasma actuator
  26. Plasma-Actuator Burst-Mode Frequency Effects on Leading-Edge Flow-Separation Control at Reynolds Number 2.6×105
  27. Characteristic finite-difference WENO scheme for multicomponent compressible fluid analysis: Overestimated quasi-conservative formulation maintaining equilibriums of velocity, pressure, and temperature
  28. Study on the Sensing Parameters toward Better Feed-back Control of Stall Separation with DBD Plasma Actuator
  29. Experimental Study on the Detailed Structure of Separation Bubble in Flow Control with DBD Plasma Actuator
  30. Burst-Mode Frequency Effects of Dielectric Barrier Discharge Plasma Actuator for Separation Control
  31. Large-Eddy Simulation of NACA 0015 Airfoil Flow at Reynolds Number of 1.6×106
  32. Spanwise modulation effects of local body force on downstream turbulence growth around two-dimensional hump
  33. Experimental Study of Burst Ratio Effect for Dielectric-Barrier-Discharge Plasma Actuator for Separation Control
  34. Control of dynamic flowfield around a pitching NACA633−618 airfoil by a DBD plasma actuator
  35. Conservative high-order flux-reconstruction schemes on moving and deforming grids
  36. Computational analysis of aeroacoustic noise generated from a rotating tire with a longitudinal groove
  37. Analysis of nozzle geometry effect on supersonic jet noise using Schlieren
  38. Multi-Objective Aeroacoustic Design Exploration of Launch-Pad Flame Deflector Using Large-Eddy Simulation
  39. Control of Dynamically Stalled Flowfield around a Pitching Airfoil by DBD Plasma Actuator
  40. Control of Airfoil Flow at Cruise Condition by DBD Plasma Actuator - Sophisticated Airfoil vs. Simple Airfoil with Flow Control -
  41. Mach Number Dependence on Sound Sources in High Mach Number Turbulent Mixing Layer
  42. Effects of Disturbed Nozzle-exit Boundary Layers on Acoustic Waves from Ideally-expanded Supersonic Jet
  43. Plate-Angle Effects on Acoustic Waves from Supersonic Jets Impinging on Inclined Plates
  44. Significance of Computational Spanwise Domain Length on LES for the Flowfield with Large Vortex Structure
  45. Experimental Study of Effects of Frequency for Burst Wave on a DBD Plasma Actuator for Separation
  46. High-speed jet noise
  47. Wall-Turbulence Structure with Pressure Gradient Around 2D Hump
  48. Computational Analysis of Compressible Gas-Particle-Multiphase Turbulent Mixing Layer in Euler-Euler Formulation
  49. Linear Stability Analyses and Large Eddy Simulations for Acoustic Wave Generation Mechanism of a Transitional Supersonic Jet
  50. Two- and Three-Dimensional Numerical Analysis for Flow Field Characteristics at Various Low Reynolds Numbers
  51. Computational Studies on Flow Separation Controls at Relatively Low Reynolds Number Regime
  52. Mechanisms for laminar separated-flow control using dielectric-barrier-discharge plasma actuator at low Reynolds number
  53. Separation control based on turbulence transition around a two-dimensional hump at different Reynolds numbers
  54. Multifactorial Effects of Operating Conditions of Dielectric-Barrier-Discharge Plasma Actuator on Laminar-Separated-Flow Control
  55. Contribution of large-scale vortex and fine-scale turbulent structure in separated flow control using DBD plasma actuator
  56. Nozzle-to-Ground Distance Effect on Nondominated Solutions of Multiobjective Aeroacoustic Flame Deflector Design Problem
  57. Fully-conservative High-order FR Scheme on Moving and Deforming Grids
  58. A Finite Difference WENO Scheme Maintaining Velocity, Pressure and Temperature Equilibrium in Multicomponent Compressible Fluid Analysis
  59. A ranking method based on two preference criteria: Chebyshev function and ε-indicator
  60. LES of transient flows controlled by DBD plasma actuator over a stalled airfoil
  61. Mechanisms of surface pressure distribution within a laminar separation bubble at different Reynolds numbers
  62. Design Exploration of a DBD Plasma Actuator for Massive Separation Control
  63. LES of Separated-flow Controlled by DBD Plasma Actuator around NACA 0015 over Reynolds Number Range of 10^4-10^6
  64. Spatial Growth of the Spanwise Disturbance Induced by a Synthetic Jet on Separation Control over an Airfoil
  65. Multiobjective Design Exploration of a Many-objective Space Trajectory Problem for Low-Thrust Spacecraft Using MOEA with Large Populations
  66. Anion and cation dynamics of sulfonylamide-based ionic liquids and the solid–liquid transitions
  67. Comparison of Numerical Methods Evaluating Airfoil Aerodynamic Characteristics at Low Reynolds Number
  68. Generation of Acoustic Disturbances in Supersonic Laminar Cavity Flows
  69. A new technique for freestream preservation of finite-difference WENO on curvilinear grid
  70. Computational and experimental analysis of flow structures induced by a plasma actuator with burst modulations in quiescent air
  71. On the freestream preservation of high-order conservative flux-reconstruction schemes
  72. Relation Between Sound Sources and Vortical Structures in Isotropic Compressible Turbulence
  73. Computational and Experimental Analysis of a High-Performance Airfoil Under Low-Reynolds-Number Flow Condition
  74. High-performance computing-based exploration of flow control with micro devices
  75. Many-objective evolutionary computation for optimization of separated-flow control using a DBD plasma actuator
  76. Effective Mechanisms for Turbulent-separation Control by DBD Plasma Actuator around NACA0015 at Reynolds Number 1,600,000
  77. LES on Turbulent Separated Flow around NACA0015 at Reynolds Number 1,600,000 toward Active Flow Control
  78. Geometric interpretations and spatial symmetry property of metrics in the conservative form for high-order finite-difference schemes on moving and deforming grids
  79. A simple interface sharpening technique with a hyperbolic tangent function applied to compressible two-fluid modeling
  80. Experimental Study of a Nano-second Pulse Plasma Actuator for Low Reynolds Number Flow Control
  81. Effect of Burst Frequency and Reynolds Number on Flow Control Authority of DBD Plasma Actuator on NACA0012 Airfoil
  82. Effects of Burst Frequency and Momentum Coefficient of DBD Actuator on Control of Deep-stall Flow around NACA0015 at Rec=2.6x10^{5}
  83. Multiobjective Design Exploration of an Aeroacoustic Design Problem for Rocket Launch Site with Evolutionary Computation and Large Eddy Simulations
  84. Computational Prediction of Acoustic Waves from a Subscale Rocket Motor
  85. Computational Analysis of Aerodynamic Performance of Mars Airplane
  86. Planetary Atmosphere Wind Tunnel Tests on Aerodynamic Characteristics of a Mars Airplane Scale Model
  87. Control surface effectiveness of low Reynolds number flight vehicles
  88. Analysis of Owl-like Airfoil Aerodynamics at Low Reynolds Number Flow
  89. Institute of Theoretical and Applied Mechanics - Place for Human Resources for Innovation and Imagination
  90. Robust explicit formulation of weighted compact nonlinear scheme
  91. Mach-Number Effects on Vortex Breakdown in Subsonic Flows over Delta Wings
  92. Scaling Analysis of Propeller-Driven Aircraft for Mars Exploration
  93. Mechanism of controlling supersonic cavity oscillations using upstream mass injection
  94. DBD Plasma Actuator Multi-Objective Design Optimization at Reynolds Number 63,000: Baseline Case
  95. Plasma Flow Control Simulation of an Airfoil of Wind Turbine at an Intermediate Reynolds Number
  96. Large-Eddy Simulations of Owl-Like Wing Under Low Reynolds Number Conditions
  97. A New Technique for Finite Difference WENO with Geometric Conservation Law
  98. Effect of Wing Planform on Aerodynamic Characteristics at Low Reynolds Numbers using a Low Density Wind Tunnel
  99. Significance of Three-dimensional Unsteady Flows inside the Cavity on Separated-flow Control around an NACA0015 using a Synthetic Jet
  100. Massive Parametric Study by LES on Separated-flow Control around Airfoil using DBD Plasma Actuator at Reynolds Number 63,000
  101. Space trajectory design: Analysis of a real-world many-objective optimization problem
  102. Effects of Inflow Shear Layer Parameters on a Transitional Supersonic Jet with a Moderate Reynolds Number
  103. On the feedback mechanism in supersonic cavity flows
  104. Control Mechanism of Plasma Actuator for Separated Flow around NACA0015 at Reynolds Number 63,000 -Separation Bubble Related Mechanisms-
  105. A non-equilibrium dynamic wall-model for LES of high Reynolds number airfoil flow near stall condition
  106. Feedback Mechanism in Supersonic Laminar Cavity Flows
  107. A New Multiobjective Genetic Programming for Extraction of Design Information from Non-dominated Solutions
  108. An Alternative Preference Relation to Deal with Many-Objective Optimization Problems
  109. Conservative metric evaluation for high-order finite difference schemes with the GCL identities on moving and deforming grids
  110. Large-Eddy Simulation of Low-Reynolds-Number Flow Over Thick and Thin NACA Airfoils
  111. Analysis of Acoustic-Fields Generated by a Supersonic Jet Impinging on Flat and Curved Inclined Plates
  112. Burst Frequency Effect of DBD Plasma Actuator on the Control of Separated Flow over an Airfoil
  113. Computational Analysis of Vortex Structures Induced by a Synthetic Jet to Control Separated Flows
  114. Numerical (error) issues on compressible multicomponent flows using a high-order differencing scheme: Weighted compact nonlinear scheme
  115. Comparative Study of Co-flow and Counter Blowing DBD Plasma Actuators for Separated Flow over an Airfoil
  116. Noise Control of Supersonic Cavity Flow with Upstream Mass Blowing
  117. Role of RANS, Hybrid and LES for Wing Flow Simulations at Relatively Low Reynolds Numbers
  118. Computational Study of Effects of Nondimensional Parameters on Synthetic Jets
  119. Aerodynamic Design Exploration for Reusable Launch Vehicle Using Genetic Algorithm with Navier Stokes Solver
  120. An Effective Three-Dimensional Layout of Actuation Body Force for Separation Control
  121. Numerical Investigation of Asymmetric Separation Vortices over Slender Body by RANS/LES Hybrid Simulation
  122. Overexpansion Effects on Characteristics of Mach Waves from a Supersonic Cold Jet
  123. Mechanism of acoustic radiation from Supersonic Jets Impinging to Inclined Flat Plates
  124. Validation study on computational aeroacoustics of acoustic waves from sub-scale rocket plumes
  125. Aeroacoustic Waves Generated from a Supersonic Jet Impinging on an Inclined Flat Plate
  126. Effects of Plate Angles on Acoustic Waves from a Supersonic Jet Impinging on an Inclined Flat Plate
  127. Experimental Study of Effects of Frequency for Burst Wave on DBD Plasma Actuator for Separation Control
  128. Computational Study of Effects of Near-wall Turbulent Structure on Aeroacoustic Waves from a Supersonic Jet Impinging on a Inclined Plate
  129. Multidisciplinary and Multi-objective Design Exploration Methodology for Conceptual Design of a Hybrid Rocket
  130. Multiobjective Design Exploration in Space Engineering
  131. Effects of Shear-Layer Characteristic on the Feedback-loop Mechanism in Supersonic Open Cavity Flows
  132. Effective Three-dimensional Layout of Imaginary Body Force for Separation Control
  133. Mach Number Effects on Vortex Breakdown in Subsonic Flow over a Delta Wing
  134. Features of Frontier Research: Consideration from the Characteristics of Space Engineering
  135. Computational Study of Aerodynamic Characteristics of an Airfoil With DBD Plasma Actuator
  136. Three-Dimensional Wing Design Towards the Future Mars Airplane
  137. Aerodynamic Design Exploration for Reusable Launch Vehicle Using Multi-Objective Genetic Programming
  138. Large-Eddy Simulation of the Flow over a Thin Airfoil at Low Reynolds Number
  139. Aerodynamic Multiobjective Design Exploration of Flapping Wing Using a Navier–Stokes Solver
  140. Experimental Study of Blowing Direction Effects of DBD Plasma Actuator on Separation Control of Flow Around an Airfoil
  141. Computational Study of Flow Characteristics of Thick and Thin Airfoil With Implicit Large-Eddy Simulation at Low Reynolds Number
  142. An Acoustic Impedance Model for Evaluating the Ground Effect of Static-Firing Tests on a Rocket Motor
  143. Toward accurate simulation and analysis of strong acoustic wave phenomena-A review from the experience of our study on rocket problems
  144. Data Mining of Pareto-Optimal Transonic Airfoil Shapes Using Proper Orthogonal Decomposition
  145. Recent Efforts in Rocket Plume Acoustics
  146. Computational Analysis of Unsteady Flow-Field Induced by Plasma Actuator in Burst Mode
  147. Aerodynamic Shape Design of the Vertical Landing Rocket Vehicle
  148. LES Study of Feedback-loop Mechanism of Supersonic Open Cavity Flows
  149. POD of Aeroacoustic Fields of a Jet Impinging on an Inclined Plate
  150. Computational Analysis of Mach Number Effects on the Edgetone Phenomenon
  151. Freestream and vortex preservation properties of high-order WENO and WCNS on curvilinear grids
  152. Acoustic Waves from a Supersonic Jet Impinging on an Inclined Flat Plate
  153. Flow Field Data Mining of Pareto-Optimal Airfoils Using Proper Orthogonal Decomposition
  154. Computational Study of the Synthetic Jet on Separated Flow Over a Backward-Facing Step
  155. Computational Study on Effect of Synthetic Jet Design Parameters
  156. An Acoustic Impedance Model for Evaluating Ground Effect of Static-Firing Tests on Rocket Motors
  157. Data Mining of Pareto-Optimal Transonic Airfoil Shapes Using Proper Orthogonal Decomposition
  158. Effects of difference scheme type in high-order weighted compact nonlinear schemes
  159. Aerodynamic Multiobjective Design Exploration of a Flapping Airfoil Using a Navier-Stokes Solver
  160. Computational Analysis of Characteristics of Mach Wave Sources in Supersonic Free-Jets
  161. Detailed Analysis of Flat Plate Pressure Peaks Created by Supersonic Jet Impingements
  162. Improvements in the Reliability and Efficiency of Body-fitted Cartesian Grid Method
  163. Airfoil Flow Experiment on the Duty Cycle of DBD Plasma Actuator
  164. Uniform Flow Preserving Property of High Order Upwind Finite Difference Schemes on Generalized Coordinate System
  165. Propulsion by an Oscillating Thin Airfoil at Low Reynolds Number
  166. Computational Study of Frequency and Amplitude Effects on Separation Flow Control With the Synthetic Jet
  167. Numerical Analysis for Magnetic Control of Heat-Transfer and Pressure in Hypersonic Shock Wave Interference Flows
  168. Data mining of non-dominated solutions using proper orthogonal decomposition
  169. Flashback: 30 Years Numerical Fluid Mechanics and Aerodynamics in Japan, other Asian Countries and the Western Pacific Rim
  170. Mach Number and Temperature Effects on Mach Wave Emission from Supersonic Jets
  171. Development of Multi-Objective Six Sigma Approach for Robust Design Optimization
  172. CFD contributions to high-speed shock-related problems
  173. Over-expansion Effects on Mach 3.0 Supersonic Jet Acoustics
  174. Aerodynamic Characteristics of a Delta Wing at High Angles of Attack
  175. Compact Scheme with Filtering for Large-Eddy Simulation of Transitional Boundary Layer
  176. Mach Number Effect on Flowfield Over a Delta Wing in Supersonic Region
  177. Generation and Propagation of Pressure Waves from H-IIA Launch Vehicle at Lift-Off
  178. Computational Analysis of Noise Sources Inside Turbulent Boundary Layer Over a Generalized Bump
  179. Visualization and Verification Method for Failure Network Analysis of Space Launch Vehicles
  180. Computational Analysis of Supersonic Underexpanded Jets Impinging on an Inclined Flat Plate
  181. Compact Differencing and Filtering Schemes for Large-Eddy Simulation of Compressible Transitional Boundary Layer
  182. A Study on Flapping Motion for MAV Design Using Design Exploration
  183. Multi-Objective Six Sigma Approach Applied to Robust Airfoil Design for Mars Airplane
  184. Increasing Order of Accuracy of Weighted Compact Non-Linear Scheme
  185. Effective Layout of Plasma Actuators for a Flow Separation Control on a Wing
  186. Study on the Automated CFD Analysis Tools for Conceptual Design of Space Transportation Vehicles
  187. Computational Analysis of Noise Sources Inside the High Speed Flow Over a Bump
  188. Influence of Stores on the Transonic Flutter of a Delta Wing Configuration
  189. Time-Series and Time-Averaged Characteristics of Subsonic to Supersonic Base Flows
  190. Computational Analysis of Characteristics and Mach Number Effects on Noise Emission From Ideally Expanded Highly Supersonic Free-Jet
  191. Computational Aeroacoustic Analysis of Overexpanded Supersonic Jet Impingement on a Flat Plate With/Without Hole
  192. New Constraint-Handling Method for Multi-Objective and Multi-Constraint Evolutionary Optimization
  193. Effects of Plasma Actuator Layouts on a Flow Separation Control over a Wing
  194. Large-Eddy Simulation of Compressible Transitional Boundary Layer
  195. Experimental Study of Underexpanded Supersonic Jet Impingement on an Inclined Flat Plate
  196. Computational Analysis of Mach Number Effects on Edgetone
  197. A Study on Airfoil Design for Future Mars Airplane
  198. Time-Series and Time-Averaged Characteristics of Subsonic to Supersonic Base Flows
  199. Flow Field Analysis of Jet Impinging on an Inclined Flat Plate at High Plate Angles
  200. Computational Aerodynamic Analysis of Capsule Configurations Toward the Development of Reusable Rockets
  201. Announcements, Comments, and Acknowledgments
  202. Improvement of noise filtering and image registration methods for the Pressure Sensitive Paint experiments
  203. Progress and future prospects of CFD in aerospace—Wind tunnel and beyond
  204. Pareto-Optimality-Based Constraint-Handling Technique and Its Application to Compressor Design
  205. Computatinal Analysis of the Characteristics of Subsonic, Transonic and Supersonic Base Flows
  206. Computational Study of a Supersonic Base Flow Using Hybrid Turbulence Methodology
  207. Analysis and Prediction of Thin-Airfoil Stall Phenomena with Hybrid Turbulence Methodology
  208. PSP Measurements in the Large-Scale Transonic Wind Tunnel and Associated Image Data Processing
  209. Numerical Analysis of the Aerodynamic Characteristics of SSTO Configurations with an Aerospike Nozzle
  210. Computational Analysis of Various Factors on the Edgetone Mechanism Using High Order Schemes
  211. New Developments in Computational Fluid Dynamics
  212. Assessment of CFD Estimation of Aerodynamic Characteristics of Basic Reusable Rocket Configurations
  213. Flow Field Analysis of Under-Expanded Supersonic Jets Impinging on an Inclined Flat Plate: Analysis With PSP/Schlieren Images and CFD Simulations
  214. Visualization for CFD Research-Past and Future
  215. Library-less Realtime Visualization System and its Use
  216. Development of Postprocessing Software for PSP/TSP Pressure Measurement System
  217. B303 感圧・感温塗料を用いた斜め平板衝突噴流の解析
  218. Effect of the Time Stepping Size in the Implicit Method for Transonic Flutter Simulations
  219. Development of Realistic Optimization Method of TSTO Spaceplane - Multi-Objective and Robust Optimization
  220. Numerical Investigations of the Side Fence Effect on Linear Plug Nozzle Performance
  221. High-Order Compact Difference Scheme Applied to Double-Delta Wing Vortical Flows
  222. Effects of Number of Stores on the Transonic Flutter Characteristics of a Delta Wing Configuration
  223. Prediction of a Thin-Airfoil Stall Phenomenon Using LES/RANS Hybrid Methodology with Compact Difference Scheme
  224. Computational Study of a Supersonic Base Flow Using LES/RANS Hybrid Methodology
  225. Flow Field and Performance Analysis of Aerospike Nozzles with Simplified Clustered Modules
  226. PSP measurements of the pressure fields over the a complicated model configuration
  227. Computational Analysis of the Effective Secondary-Flow Injections for the Plug-Nozzle Drag Reduction
  228. Application of High-Order Compact Difference Scheme to Vortical Flow Computation over a Delta and Double-Delta Wings
  229. Flow Classification of the Under-Expanded Super Sonic Jet Impinging on a Flat Plate
  230. CFD Prediction of the Aerodynamic Characteristics of Capsule-Like Configurations for the Future SSTO Development
  231. Compressible Flow Simulations Over Basic Reusable Rocket Configurations
  232. Improvement of the Noise Filtering and Image Registration Methods for PSP Experiments
  233. Numerical Estimations of Transonic Flutter Calculation with the Fluid/Structure Coupling Method
  234. Numerical Analysis of the Clustered Type Aerospike Nozzle Flow: Flow Structures and Thrust Performance
  235. Flow Field and Performance Analysis of an Annular-Type Aerospike Nozzle with Base Bleeding.
  236. Establishment of the PSP measurement system using Ruthenium(II) complex
  237. On Post Image Processing for Pressure Sensitive Paint
  238. Mechanism of Dynamic Instability of a Reentry Capsule at Transonic Speeds
  239. Visualization of Jet Flows over a Plate by Pressure-Sensitive Paint Experiments and Comparison with CFD
  240. The Effect of Module Clustering on Aerospike Nozzle Performance
  241. Computational Analysis of the Secondary Flow Injection for the Drag Reduction of the Plug Nozzle
  242. Computations of Axisymmetric Plug-Nozzle Flowfields: Flow Structures and Thrust Performance
  243. Numerical Investigations of the Base-Flow Characteristics of Axisymmetric Aerospike Nozzles.
  244. Computational Analysis of the Flow Field Near the Boat-tail Region of Annular Plug Nozzles.
  245. On Post Image Processing for Pressure Sensitive Paint
  246. Assessment of the Reliability of CFD simulations for Delta wings Using Visualization Post Processings
  247. Computation of the Flow Field around Arbitrary Three-Dimensional Body Geometry Using Cartesian Grid.
  248. CFD Applications to Space Transportation Sytems
  249. Lessons Learned from the Blast Wave Computation Using Overset Moving Grids: Grid Motion Improves the Resolution
  250. Flow field and performance analysis of the simplified clustered aerospike nozzles
  251. Computers and flow visualization
  252. Computational analysis of the flow field near the boat-tail region of annular plug nozzles
  253. Numerical Analysis of Dynamic Stability of a Reentry Capsule at Transonic Speeds
  254. Flow field analysis of the base region of axisymmetric aerospike nozzles
  255. Real-Time Computation and Visualization on Mobile PC’s
  256. A Visualization Technique to Identify the Flow Mechanism of Complicated Unsteady Flows
  257. Numerical analysis of dynamic stability of a reentry capsule at transonic speeds
  258. PSP Measurement of the Jet Impingement Flow Field over a Flat Plate
  259. Study on the mechanism of the instability of a re-entry capsule at transonic speeds
  260. Computational study of the flow field behind blunt capsules at transonic speeds
  261. Computations of the axisymmetric plug nozzle flow fields - Flow structures and thrust performance
  262. Numerical analysis of three-dimensional shock/shock interactions and the aerodynamic heating
  263. Recent Development of Aerodynamic Design Methodologies
  264. Efficiency improvement of unified implicit relaxation/time integration algorithms
  265. Efficiency Improvement of Unified Implicit Relaxation/Time Integration Algorithms
  266. 論文「Roeの近似Riemann solverの収束性に関する一考察」に対する質問
  267. COMPUTATIONS OF BLAST WAVE PROPAGATION USING AN OVERSET MOVING ZONAL METHOD
  268. What Have We Learned from Computational Fluid Dynamics Research on Train Aerodynamics?
  269. Prediction Method of Unsteady Combustion Around Hypersonic Projectile in Stoichiometric Hydrogen-Air
  270. Three-Dimensional Flow Computation Around a Projectile Overtaking a Preceding Shock Wave
  271. Numerical analysis of dynamic stability of a reentry capsule at transonic speeds
  272. Prediction method of unsteady combustion around hypersonic projectile in stoichiometric hydrogen-air
  273. Numerical investigation of three-dimensional compressible flows induced by a train moving into a tunnel
  274. Numerical investigation of the one-dimensional piston supported detonation waves
  275. Efficiency improvements of unified implicit relaxation/time integration algorithms and their applications
  276. Three-dimensional computation of the flow induced by a projectile overtaking a shock wave
  277. Cavity Flow with a Shock Wave Interaction in a Supersonic Duct.
  278. Numerical Analysis of a Three-Dimensional Cavity Flow Field in a Supersonic Duct.
  279. Detailed mechanism of the unsteady combustion around hypersonic projectiles
  280. Enhancement of the leading-edge separation vortices by trailing-edge lateral blowing
  281. First Damkoehler parameter for prediction and classification of unsteady combustions around hypersonic projectiles
  282. Unsteady behavior of the shock wave passing over two and three dimensional obstacles
  283. Flow Visualization in Computational Fluid Dynamics.
  284. Flow Characteristics around the Cavity in a Supersonic Duct.
  285. Theoretical Algorithm to Design a Train Shape for Alleviating the Booming Noise at a Tunnel Exit.
  286. Aerodynamics of high speed trains passing by each other
  287. Computational study of large-disturbance oscillations in unsteady supersonic combustion around projectiles
  288. Examination of the improved model for the unsteady combustion around hypersonic projectiles
  289. Experimental investigation of supersonic internal cavity flows
  290. Three-dimensional adaptive bisection of unstructured grids for transient compressible flow computations
  291. Numerical simulation of the flow around a projectile passing through a shock wave
  292. Flow features of shock-induced combustion around projectile traveling at hypervelocities
  293. Unified Zonal Method Based on the Fortified Solution Algorithm
  294. Numerical investigation of supersonic flows around a spiked blunt body
  295. Prediction of Wavefront of Compression Wave Generated by a Train Moving into a Tunnel with Steady Flow.
  296. On-dimensional Numerical Simulation of a Compression Wave Induced by a Train Entering a Tunnel.
  297. Enhancement of the leading-edge separation vortices by the trailing-edge lateral blowing
  298. Computational study of unsteady combustion around projectiles with emphasis on the large-disturbance oscillation
  299. SIMULATION OF EXPERIMENTAL VISUALIZATION METHODS FOR COMPUTATIONAL FLUID DYNAMICS RESEARCH
  300. Conservation law for moving and transformed grids
  301. Numerical experiment of the flight trajectory simulation by fluid dynamics and flight dynamics coupling
  302. Numerical Simulation of Compressible Flow Induced by a Train Moving in a Tunnel
  303. Nonequilibrium turbulence modeling study on light dynamic stall of aNACA0012 airfoil
  304. Flow features of shock-induced combustion around projectile travelling at hypervelocities
  305. Numerical investigation of supersonic flows around a spiked blunt-body
  306. Supercomputers and Their Performance in Computational Fluid Dynamics
  307. Navier-Stokes Benchmark Tests
  308. Visualization Technique in Computational Fluid Dynamics for Rational Comparison with Experiment
  309. Recent Applications of the FNS Zonal Method to Complex Flow Problems
  310. Numerical Simulations of Hypersonic Real-Gas Flows Over Space Vehicles
  311. Unified zonal method based on the fortified Navier-Stokes concept
  312. Supersonic inlet flow computations using fortified Navier-Stokes approach
  313. Navier-Stokes simulation of two and three dimensional jets in crossflow
  314. Numerical Simulation and Visualization for High Speed Flows
  315. Visualization for computational fluid dynamics and the comparison with experiments
  316. Newly constructed high speed wind tunnel at the Institute of Space and Astronautical Science (ISAS) and related activities
  317. Supercomputers and Workstations in Fluid Dynamic Research
  318. High-resolution upwind scheme for vortical-flow simulations
  319. Numerical simulation of vortical flows over a strake-delta wing
  320. Navier-Stokes computations of the supersonic flows about a Space-Plane
  321. Use of high-resolution upwind scheme for vortical flow simulations
  322. Numerical study of the effect of tangential leading edge blowing on delta wing vortical flow
  323. Computational fluid dynamics: Recent topics and the trend.
  324. A method to increase the accuracy of vortical flow simulations
  325. Navier Stokes computation of the flow field over delta wings with spanwise leading edge blowing
  326. Numerical Aerodynamic Simulation Facility Takes Off
  327. Navier-Stokes simulations of transonic flows over a wing-fuselage combination
  328. Numerical simulation of vortical flows over a strake-delta wing
  329. Toward the Navier-Stokes analysis of transport aircraft configurations
  330. Navier-Stokes computations of transonic flows using the LU-A
  331. Navier-Stokes simulations of transonic flows over a practical wing configuration
  332. Viscous Compressible Flow Simulations Using Supercomputers
  333. Computation of viscous transonic flows about aircrafts and its visulization.
  334. Recent computational fluid dynamics works about high angle of attack aerodynamics with separations vortex.
  335. Computational Fluid Dynamics Study at NASA Ames Research Center
  336. Accurate simulation of vortical flows
  337. Improvement of the Optimization Method of the TSTO Configuration — Application of Accurate Aerodynamics
  338. Numerical Approach to the Analysis of Internal Pressure of M–V Rocket Fairing
  339. Simultaneous solutions of inviscid flow and boundary layer at transonic speeds
  340. An efficient four-factored time integration scheme for three-dimensional compressible flow problems
  341. Simulations of unsteady shock wave reflections using adaptive unstructured grids
  342. Visualization method for computational fluid dynamics with emphasis on the comparison with experiments