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Full Length Papers(Scramjet)(2012)
2012・Error Analysis on Multi-Fidelity Design Spaces through Surrogate Modeling with an Emphasis on Scramjet Combustion
・LES-based Eulerian PDF approach for the simulation of scramjet combustors
・Cyber-Based Turbulent Combustion Simulation
・Uncertainty in velocity measurement based on diode-laser absorption in nonuniform flows
・ROBUST DESIGN OPTIMIZATION OF HIGH-PERFORMANCE AXISYMMETRIC SCRAMJETS BASED ON SURROGATE-ASSISTED EVOLUTIONARY ALGORITHMS
・Trajectory Analysis of Fuel Injection into Supersonic Cross Flow Based on Schlieren Method
・SUPERSONIC COMBUSTION RAMJET RESEARCH
・Large-Eddy Simulation of a Supersonic Inlet-Isolator
・Effects of Angles of Attack and Throttling Conditions on Supersonic Inlet Buzz
・COMPUTATIONAL INVESTIGATION OF THE EFFECT OF NOSE BLUNTNESS ON THE EXTERNAL AND INTERNAL COMPRESSION IN A MIXED INLINE INTAKE
・Hypersonic inlet for a laser powered propulsion system
・Shock-less Hypersonic Intakes
・Collaborative Research: Advanced Excimer Laser Measurements and LES Modeling of Supersonic Combustion
・(AIAA JOURNAL Vol. 50, No. 3, March 2012)Risk Assessment of Scramjet Unstart Using Adjoint-Based Sampling Methods
・(AIAA2012-5975)Analysis of a Three-Dimensional, High Pressure Ratio Scramjet Inlet with Variable Internal Contraction
・(AIAA2012-5913)Investigation of Unsteady/Quasi-Steady Scramjet Behavior using High-Speed Visualization Techniques
・(AIAA2012-5909)Sensitivity of Flight Dynamics of Hypersonic Vehicles to Design Parameters
・(AIAA2012-5878)A Thermal Analysis Method for Fuel-Cooled Combustor Structure based on Heat Flux Measurement
・(AIAA2012-5876)Pyrolysis in Porous Media:Numerical model and parametric study.
・(AIAA-RS-2012-5001)Responsive and Affordable Launch of Small Satellites: A Reusable Air-breathing Concept
・(AIAA2012-4958)Continuous Differentiation of Complex Systems Applied to a Hypersonic Vehicle
・(AIAA2012-4264)Progress Toward Affordable High Fidelity Combustion Simulations for High-Speed Flows in Complex Geometries
・(AIAA2012-4263)Low-Dissipation Advection Schemes Designed for Large Eddy Simulations of Hypersonic Propulsion Systems
・(AIAA2012-4262)Large-Eddy / Reynolds-Averaged Navier-Stokes Simulations of Scramjet Combustor Flow Fields
・(AIAA2012-4161)Integrated Analysis for the Design of Reusable TPS based on Variable Transpiration Cooling for Hypersonic Cruise Vehicles
・(AIAA2012-4149)A Turbine Based Combined Cycle Engine Inlet Model and Mode Transition Simulation Based on HiTECC Tool
・(AIAA2012-4144)A Framework for Simulating Turbine-Based Combined-Cycle Inlet Mode-Transition
・(AIAA2012-4143)Highlights from a Mach 4 Experimental Demonstration of Inlet Mode Transition for Turbine-Based Combined Cycle Hypersonic Propulsion
・(AIAA2012-4090)Quasi-1D Compressible Flow of Hydrocarbon Fuel
・(AIAA2012-3924)Study of Forebody Injection and Mixing with Application to Hypervelocity Airbreathing Propulsion
・(AIAA2012-3848)Visualization of Vaporized Kerosene Combustion in a Supersonic Combustor Using Pulsed Schlieren System
・(AIAA2012-3762)Characteristics of a Supersonic Model Combustor with Two-Staged Injections of Supercritical Kerosene
・(AIAA2012-3707)Current Status of Superheat Spray Modeling With NCC
・(AIAA2012-3292)A General Simulation of an Air Ejector Diffuser System
・(AIAA2012-3285)Simulation of a Wall-Bounded Flow using a Hybrid LES/RAS Approach with Turbulence Recycling
・(AIAA2012-3264)A study of expansion tube gas flow conditions for scramjet combustor model testing
・(AIAA2012-3252)A numerical method for DNS of turbulent reacting fows using complex chemistry
・(AIAA2012-3224)Studies of Inlet Distortion in a Direct-Connect Axisymmetric Scramjet Isolator
・(AIAA2012-3199)Measurement of Vibrational Non-equilibrium in a Supersonic Freestream using Dual-Pump CARS
・(AIAA2012-3147)Boundary-Layer Instability Measurements in a Mach-6 Quiet Tunnel
・(AIAA2012-2887)OH PLIF Visualization of the UVa Supersonic Combustion Experiment: Configuration A
・(AIAA2012-2751)Thermal Radiative Analysis of the HIFiRE-2 Scramjet Engine
・(AIAA2012-1241)Free-flight force measurement technique in shock tunnel
・(AIAA2012-1193)Development of a Dual-Pump CARS System for Measurements in a Supersonic Combusting Free Jet
・(AIAA2012-0972)A Method to Image Flame Index in Partially Premixed Flames
・(AIAA2012-0947)Dual-Mode Scramjet Combustor: Numerical Sensitivity and Evaluation of Experiments
・(AIAA2012-0857)Optical Measurements at the Combustor Exit of the HIFiRE 2 Ground Test Engine
・(AIAA2012-0789)Experimental Investigations of High Voltage Pulsed Pseudospark Discharge and Intense Electron Beams
・(AIAA2012-0611)LES/RANS Simulation of a Supersonic Combustion Experiment
・(AIAA2012-0566)Multi-Scale Turbulence Model in Simulation of Supersonic Crossflow Part 2: Inclined Injection
・(AIAA2012-0482)Large Eddy Simulation based Studies of Reacting and Non-reacting Transverse Jets in Supersonic Crossflow
・(AIAA2012-0481)Hypervelocity Testing of a Dual-mode Scramjet
・(AIAA2012-0447)Effect of subharmonic forcing on transition in chemically reactive shear-layers
・(AIAA2012-0333)Supersonic Combustion and Flame-Holding Characteristics of Pylon Injected Hydrogen in a Mach 2.4 High Enthalpy Flow
・(AIAA2012-0332)Evolution of Large-Scale Structures Generated by a Strut Injector in a Mach 2.5 Flow
・(AIAA2012-0330)AN INVESTIGATION OF A SCRAMJET CAVITY FLAMEHOLDER USING STEREOSCOPIC PARTICLE IMAGE VELOCIMETRY
・(AIAA2012-0282)Hypersonic Boundary-Layer Transition Experiments in the Boeing/AFOSR Mach-6 Quiet Tunnel
・(AIAA2012-0255)Longitudinal flight dynamics modelling and control of ScramSpace I
・(AIAA2012-0180)Sensitivity analysis for Eulerian PDF methods
・(AIAA2012-0151)PDE-constrained optimization with error estimation and control
・(AIAA2012-0115)Large-Eddy / Reynolds-Averaged Navier-Stokes Simulations of a Dual-Mode Scramjet Combustor
・(AIAA2012-0113)Close-Collaborative Experimental and Computational Study of a Dual-Mode Scramjet Combustor
・(AIAA2012-0112)Development of Methods to Predict High-Speed Reacting Flows in Aerospace Propulsion Systems