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Full Length Papers(Scramjet)(2011)
2011・YIP-08 Hypervelocity Boundary Layer Studies for Axisymmetric Engine Flowpaths
・Plasma-assisted ignition and deflagration-to-detonation transition
・Simultaneous measurements of multiple flow parameters for scramjet characterization using tunable diode-laser sensors
・Diode laser sensor for scramjet inlets: final year report
・A realizable multivariate quadrature based approach for supersonic combustion modeling in LES
・Continuous and Discrete Adjoints to the Euler Equations for Fluids
・PTAH-SOCAR FUEL-COOLED COMPOSITE MATERIALS STRUCTURE : 2011 STATUS
・TASCOM3D - A Scientific Code for Compressible Reacting Flows
・A study of expansion tube gas flow conditions for scramjet combustor model testing
・Large-Eddy Simulations of Scramjet Engines
・Preliminary Numerical Analysis of the LAPCAT MR2 Vehicle Configuration at Mach 8 Cruise Conditions
・Revolutionary Materials for Hypersonic Flight
・A Shape-Morphing Ceramic Composite for Variable Geometry Scramjet Inlets
・Proceedings of The High Performance Computing Modernization Program Users Group Conference 2011
・Transition and Turbulence Modeling
・Numerical Investigation of Fundamental Physics for Flows over Expansion and Compression Corners
・Numerical Investigations of Relaminarization in Scramjet Flows
・A Shape-Morphing Ceramic Composite for Variable Geometry Scramjet Inlets
・Experimental results of a Mach 10 conical-fl ow derived waverider to 14-X hypersonic aerospace vehicle
・Wall-modeled large eddy simulation of scramjet combustion
・Classifier utility modeling and analysis of hypersonic inlet start/unstart considering training data costs
・(AIAA2011-6942)The U.S. Navy’s Contribution to Airbreathing Missile Propulsion Technology
・(AIAA2011-6378)E ect of Control Surface-Fuselage Inertial Coupling on Hypersonic Vehicle Flight Dynamics
・(AIAA2011-6300)Turn Performance of an Air-Breathing Hypersonic Vehicle
・(AIAA2011-6229)Impact of Plume Modeling on the Design and Control for a Class of Air-Breathing Hypersonic Vehicles
・(AIAA2011-6227)Control Oriented Modeling of 6-DOF Hypersonic Vehicle Dynamics
・(AIAA2011-6108)Measurements of the Blowout Limits of Supercritical Aviation Kerosene in a Supersonic Combustor
・(AIAA2011-6107)Experimental Study on the Flame Holding Torch of a Hydrocarbon Fueled Combined Supersonic Combustor with a Pilot Burner and a Streamwise-Vortices Generator
・(AIAA2011-6106)Kinetic Modeling of Thermal and Catalytic Cracking of Paraffinic Surrogate Fuels Relevant to Hypersonic Applications
・(AIAA2011-5919)Theoretical and Numerical analysis of the Turbulence scaling in Supersonic
・(AIAA2011-5916)Measurements of Wall Heat Flux and Temperature in a Supersonic Model Combustor
・(AIAA2011-5915)Research on Combustion of Ethylene in a Supersonic Combustor
・(AIAA2011-5853)A Quasi Global Mechanism of Kerosene Combustion for Propulsion Applications
・(AIAA2011-5850)A New Method of Chemical Kinetic Model Reduction for CFD Applications
・(AIAA2011-5830)Effect of Fuel Injection Locations with a Hyper Mixer in Supersonic Combustion
・(AIAA2011-5829)Role of Turbulence Modeling in Supersonic Combustion
・(AIAA2011-5825)Analysis of Hybrid LES / RANS Simulations of a Back-Pressured Supersonic Isolator
・(AIAA2011-5790)Study of Unsteady, Sphere-Driven, Shock-Induced Combustion for Application to Hypervelocity Airbreathing Propulsion
・(AIAA2011-5765)On Cross-flow Mixing Parameters in Presence of Pseudo-Shock Wave System
・(AIAA2011-5674)Large-Eddy Simulations of Hydrogen and Ethylene Injections into a Supersonic Crossflow
・(AIAA2011-5762)Dynamics, Disruption, and Vaporization of Droplets under Supersonic Conditions
・(AIAA2011-5760)Freestream Disturbance E ects on an Axisymmetric Hypersonic Intake
・(AIAA2011-5757)Multidisciplinary Optimization of the Fuel Consumption of a Dual Mode Scramjet-Ramjet
・(AIAA2011-5756)Performance Analysis of Variable-Geometry Scramjet Inlets Using a Low-Order Model
・(AIAA2011-5723)Hypersonic Inlet Research for Small Earth-to-Orbit Vehicles Propelled by Laser Beams
・(AIAA2011-5691)A Computational Method for Combustion in Supersonic Flows
・(AIAA2011-5641)Nonlinear Energy Transfer Applied to Data Analysis in Combustion Instability
・(AIAA2011-5635)Nonlinear Dynamic Modeling and Controls Development for Supersonic Propulsion System Research
・(AIAA2011-5600)Thermometry and Velocimetry in Supersonic Flows via Scanned Wavelength-Modulation Absorption Spectroscopy
・(AIAA2011-5547)Pulsed Combustion of Hydrocarbon Fuels in a Supersonic Model Combustor
・(AIAA2011-5543)DES Study of H2+CO Turbulent Combustion with Supersonic Coflow Air at Elevated Enthalpy Condition
・(AIAA2011-5542)High Fidelity Analysis of a Generic Supersonic Combustor with a Single Open Cavity
・(AIAA2011-5540)Simulations of Inlet Distortion Effects in a Direct-Connect Scramjet Isolator
・(AIAA2011-3936)Experimental and Computational Studies of Mixing in Supersonic Flow
・(AIAA2011-3909)Geometrical shock dynamics and engine unstart
・(AIAA2011-3889)Measurement of surface pressure fluctuation in hypersonic high-enthalpy boundary layer on a 7-degree cone model
・(AIAA2011-3877)Experimental Study of Second-Mode Instabilities on a 7-Degree Cone at Mach 6
・(AIAA2011-3876)Experimental Study of Mach 6 Boundary Layer Response to Laser Generated Disturbances
・(AIAA2011-3848)Student Paper Competition:A Numerical Study of Filtering and Control for Scramjet Engine Flow
・(AIAA2011-3744)Flow Settling over a Wedge at the MHD-Effect on a Hypersonic Air Flow
・(AIAA2011-3736)Effect of Impulsive Plasma Discharge in Hypersonic Boundary Layer over Flat Plate
・(AIAA2011-3714)Numerical Simulation of Flow in a Dual-Mode Scramjet Combustor
・(AIAA2011-3713)Pulsed Detonation Combustor in a Supersonic Cross-Flow for Enhanced Mixing and Ignition
・(AIAA2011-3712)Supersonic combustion of hydrocarbon pyrolysed coolant with detailed chemistry.
・(AIAA2011-3702)Adaptive Turbulent Schmidt Number Approach for Multi-Scale Simulation of Supersonic Crossflow
・(AIAA2011-3690)On Further Development of an Unstructured Space-Marching Technique
・(AIAA2011-3599)Three-dimensional Numerical Simulation of Cylindrical Shaped Magnetohydrodynamic Generator under Strong Magnetohydrodynamic Interaction
・(AIAA2011-3598)Numerical Analysis of Generator Performance of Experimental DCW-MHD Generators with Circular and Square Cross-Section
・(AIAA2011-3597)Conceptual Design and Three-dimensional Analysis for Commercial-Scale Faraday-Type MHD Generator
・(AIAA2011-3595)Hypersonic Vehicle MHD Power Extraction Concept Utilizing Mach Stem Thermal Ionization
・(AIAA2011-3591)Flow Matching Results of an MHD Energy Bypass System on a Supersonic Turbojet Engine using the Numerical Propulsion System Simulation (NPSS) Environment
・(AIAA2011-3464)Experimental Investigations on a Hypersonic Nitrogen Flow for Magneto Fluid Dynamic Interaction around a Blunt Body
・(AIAA2011-3447)Simulation of active species production in nonequilibrium discharge plasmas
・(AIAA2011-3431)Large-Eddy Simulation of a Mach 2.9 Turbulent Boundary Layer over a 24°Compression Ramp
・(AIAA2011-3429)Turbulence Measurements with PIV in a Hypersonic Shock Boundary Layer Interaction
・(AIAA2011-3428)Experiments on the In uence of a Microramp Array on a Hypersonic Shock Turbulent Boundary Layer Interaction
・(AIAA2011-3415)Recommendations for Hypersonic Boundary Layer Transition Flight Testing
・(AIAA2011-3400)Validation of SPHC and CRASH codes in modeling of linear and non-linear Richtmyer-Meshkov instabilities
・(AIAA2011-3363)Comparison of Stability of Hypersonic Rectangular and Three-Dimensional Inlets to Unsteady Perturbations Using Entropy Considerations
・(AIAA2011-3325)A Vision of Quantitative Imaging Technology for Validation of Advanced Flight Technologies
・(AIAA2011-3248)Roughness-Induced Instabilities at Mach 6: A Combined Numerical and Experimental Study
・(AIAA2011-3215)Supersonic combustion studies using a multivariate quadrature based method for combustion modeling
・(AIAA2011-3213)Simulation of Unsteady Shock-Induced Combustion Using Hybrid Eulerian-Lagrangian Formulation
・(AIAA2011-3211)Numerical Simulation of Supersonic Chemically Reacting Turbulent Jets
・(AIAA2011-3192)Experimental and Computational Investigation of Mass Injection Induced Unstart
・(AIAA2011-3146)Implementation of a Newton Method for the Rapid Propagation of Thermochemical Model Uncertainty in Hypersonic Flows
・(AIAA2011-3143)Shock Wave Impingement on Boundary Layers at Hypersonic Speeds: Computational Analysis and Uncertainty
・(AIAA2011-3142)Uncertainty Assessments of 2D and Axisymmetric Hypersonic Shock Wave - Turbulent Boundary Layer Interaction Simulations at Compression Corners
・(AIAA2011-2397)Combined Cycle Propulsion:Aerojet Innovations for Practical Hypersonic Vehicles
・(AIAA2011-2396)Modelling of Self-Ignition Processes in Supersonic Non Premixed Coflowing Jets Based on a PaSR Approach
・(AIAA2011-2395)Numerical Investigation of Combustion/Shock-train Interactions in a Dual-Mode Scramjet Engine
・(AIAA2011-2394)Uncertainty Propagation in Integrated Airframe-Propulsion System Analysis for Hypersonic Vehicles
・(AIAA2011-2392)AN OVERVIEW OF NASA'S INTEGRATED DESIGN AND ENGINEERING ANALYSIS (IDEA) ENVIRONMENT
・(AIAA2011-2382)Numerical Simulation of Complex Internal Viscous Flow in the HyShot-II Scramjet Model
・(AIAA2011-2380)Design of Dual-Mode Engine Flowpaths for Hypersonic Vehicles Using Reduced-Order Models
・(AIAA2011-2377)Design Methodology for the Airbreathing Second Stage of a Rocket-Scramjet-Rocket Launch Vehicle
・(AIAA2011-2374)Experimental investigation of hypersonic boundary-layer transition on a cone model in the High Enthalpy Shock Tunnel (HEG) at Mach 7.5
・(AIAA2011-2370)Orbiter Trajectory Analysis for a Two-Stage Reusable Launch Vehicle
・(AIAA2011-2368)Flight Envelope Calculation of a Hypersonic Vehicle Using a First Principles-Derived Model
・(AIAA2011-2364)Mixing and turbulent kinetic Energy scaling in compressible reacting flows
・(AIAA2011-2360)Plasma Control of an Unstarting Supersonic Flow
・(AIAA2011-2359)Post-Flight Analysis of the Diode-Laser-Based Mass Capture Experiment Onboard HIFiRE Flight 1
・(AIAA2011-2350)Experimental Investigation on the Influence of Sidewall Compression on the Flowfield of a Scramjet Inlet at Mach 7
・(AIAA2011-2349)The Influence of Boundary Layers on Supersonic Inlet Unstart
・(AIAA2011-2348)Experiment of Dynamic Angle-of-Attack on a Side Wall Compression Scramjet Inlet at Mach 3.85
・(AIAA2011-2344)Hybrid Reynolds-Averaged and Large-Eddy Simulation of Scramjet Fuel Injection
・(AIAA2011-2342)Streamwise Vortices Introduced by "Hyper-Mixer" on Supersonic Mixing
・(AIAA2011-2338)Rocket Based Combined Cycle Hypersonic Vehicle Design for Orbital Access
・(AIAA2011-2336)Structural Analysis of the LAPCAT-MR2 Waverider Based Vehicle
・(AIAA2011-2332)Investigations on Multi-Stage Supersonic Combustion in a Model Combustor
・(AIAA2011-2331)The Effect of Suction Tunnel Parameters on the Concordant Control of Inlet/SERN of the Off-design Scramjet
・(AIAA2011-2327)Plasma-Based Fast Mixing and Ignition in Supersonic Flow
・(AIAA2011-2326)Characteristics of Supersonic Combustion with Hartmann-Sprenger Tube Aided Fuel Injection
・(AIAA2011-2319)Preliminary Design of a Hypersonic Air-breathing Vehicle
・(AIAA2011-2317)LAPCAT-II : conceptual design of a Mach 8 TBCC civil aircraft, enforced by full Navier-Stokes 3D nose-to-tail computation
・(AIAA2011-2314)Applications of 3-Dimensional Effect of Shock Waves caused by a Strut-Cowl System in a Scramjet Engine
・(AIAA2011-2313)Numerical and experimental scientific investigation of combustion in a translating cowl dual-mode ramjet
・(AIAA2011-2312)PIV Experimental and Numerical Investigation of Cold Flowfield of Scramjet Combustor with Inlet/Isolator
・(AIAA2011-2311)Experimental Characterization of Hydrocarbon-Fueled, Axisymmetric Scramjet Combustor Flowpaths
・(AIAA2011-2310)An Experimental Investigation of Steady and Unsteady Combustion Phenomena in the HyShot II Combustor
・(AIAA2011-2309)CFD Analysis of Unstart Characteristics of the HyShot II Scramjet Configuration in the HEG Shock Tunnel
・(AIAA2011-2308)A Novel Test of Starting Characteristics of Hypersonic Inlets in Shock Tunnel
・(AIAA2011-2307)Principle of Minimum Entropy Analysis Applied to Unsteady Flow in Hypersonic Three-Dimensional Inlets
・(AIAA2011-2295)The Hypersonic Space and Global Transportation System: A Concept for Routine and Affordable Access to Space
・(AIAA2011-2293)The Simulation of Combustion Flow of the Supersonic Combustion Chamber
・(AIAA2011-2292)Supersonic Decelerators for Freeflight Atmospheric Flight Testing
・(AIAA2011-2285)COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS
・(AIAA2011-2283)Uncertainty Quantification and Error Estimation in Scramjet Simulation
・(AIAA2011-2281)Progress in Multidisciplinary Analysis and Evaluation of Supersonic Combustion Ramjets
・(AIAA2011-2279)Overview of the Advanced Propulsion Test Technology Hypersonic Aero Propulsion Clean Air Testbed
・(AIAA2011-2278)A Unique, Mach 6 Enthalpy, Non-Vitiated Facility for Hypersonic Aerodynamics Research
・(AIAA2011-2277)The SCRAMSPACE I Hypersonic Flight Experiment Feasibility Study
・(AIAA2011-2275)HIFiRE 4: A Low-Cost Aerodynamics, Stability, and Control Hypersonic Flight Experiment
・(AIAA2011-2270)Numerical and experimental investigation on hypersonic inward turning inlets with basic flowfield using arc tangent curve law of pressure rise
・(AIAA2011-2268)Numerical Parametric Analysis of a Generic Supersonic Combustor with a Modified Single Cavity
・(AIAA2011-2267)An Efficient Flamelet-based Combustion Model for Supersonic Flows
・(AIAA2011-2256)Numerical Investigations of the E ects of Sidewall Compression and Relaminarization in 3D Scramjet Inlet
・(AIAA2011-2254)Investigation of REST-class Hypersonic Inlet Designs
・(AIAA2011-2250)Large-Eddy Simulation of Supersonic Film Cooling at Laminar and Turbulent Injection
・(AIAA2011-2249)Combustor Operability and Performance Verification for HIFiRE Flight 2
・(AIAA2011-2248)HIFiRE Direct-Connect Rig (HDCR) Phase I Scramjet Test Results from the NASA Langley Arc-Heated Scramjet Test Facility
・(AIAA2011-2247)Analysis of a Two-Staged Supersonic Combustion Chamber using Experiments and Simulations
・(AIAA2011-2243)Sustained Hypersonic Flight in Europe:First Technology Achievements within LAPCAT II
・(AIAA2011-2237)Two Steps Instead of a Giant Leap ? An Approach for Air Breathing Hypersonic Flight
・(AIAA2011-2230)Annular MHD Physics for Turbojet Energy Bypass
・(AIAA2011-2229)A Technology Pathway for Airbreathing, Combined-Cycle, Horizontal Space Launch Through SR-71 Based Trajectory Modeling
・(AIAA2011-2223)Scramjet Isolator Shock-Train Leading-Edge Location Modeling
・(AIAA2011-2222)Assessment of Isolator Pseudo-shocks Created by Combustion with Heated Flow
・(AIAA2011-2221)2-D Transient CFD Model of an Isolator Shock Train
・(AIAA2011-2216)Large Eddy Simulations of Turbulent Enhancement due to Forced Shock Motion in Shock-Boundary Layer Interaction
・(AIAA2011-2215)Steady Shock Refraction in Hypersonic Ramp Flow
・(AIAA2011-2207)Numerical Simulation of the Internal and External Flowfields of a Scramjet Fuel Strut Injector Including Conjugate Heat Transfer
・(AIAA2011-2204)Preliminary Preflight CFD Study on the HIFiRE Flight 2 Experiment
・(AIAA2011-2202)HIFIRE FLIGHT 2 OVERVIEW AND STATUS UPDATE 2011
・(AIAA2011-2059)Analysis of a Microstructure for Highly Reflective Thermal Radiation Barrier Coatings
・(AIAA2011-2037)A Surrogate Accelerated Bayesian Inverse Analysis of the HyShot II Flight Data
・(AIAA2011-1965)Fluid-Thermal-Structural Modeling and Analysis of Hypersonic Structures under Combined Loading
・(AIAA2011-1300)Validation and Verification of the Navier-Stokes Solutions Obtained from the Applications of the Integro-differential Scheme
・(AIAA2011-1294)Demonstration of Capability of Water Flux Measurement in a Scramjet Combustor using Tunable Diode Laser Absorption Tomography and Stereoscopic PIV
・(AIAA2011-1293)Spatially- and Temporally-resolved Multi-parameter Interferometric Rayleigh Scattering
・(AIAA2011-1291)Spatially Resolved Temperature and Water Vapor Concentration Distributions in a Flat Flame Burner by Tunable Diode Laser Absorption Tomography
・(AIAA2011-1289)Pressure and thermochemistry measurements in high speed flows using rotational and vibrational Raman spectroscopy
・(AIAA2011-1218)Effects of shear-layer characteristic on the Feedback-loop Mechanism in supersonic open cavity flows
・(AIAA2011-1211)Methane-Air Mixture Ignition by Combined Laser and Microwave Discharges
・(AIAA2011-1202)Numerical Model of an Aspirated Temperature Probe
・(AIAA2011-1143)Plasma Control of a Turbulent Boundary Layer in an Unstarting Supersonic Flow
・(AIAA2011-1094)Tunable Diode Laser Absorption Sensor for Measurements of Temperature and Water Concentration in Supersonic Flows
・(AIAA2011-0985)Stereoscopic Planar Laser-Induced Fluorescence Imaging at 500 kHz
・(AIAA2011-0970)Studies of C2H6/ air and C3H8/ air Plasma assisted combustion kinetics in a nanosecond discharge
・(AIAA2011-0928)NO PLIF Imaging in the CUBRC 48” Shock Tunnel
・(AIAA2011-0860)Numerical Analysis of Wall Properties in Crossing-Shock-Wave/Turbulent-Boundary-Layer Interactions
・(AIAA2011-0849)Pressure-Sensitive Paint Application on Two-Dimensional and Axisymmetric Model in Hypersonic Flow
・(AIAA2011-0773)A Parallel Matrix-Free Implicit Finite Volume Method for Chemically Reacting Flows on Hybrid Grids
・(AIAA2011-0769)Hybrid Large-Eddy Simulation / Reynolds-Averaged Navier-Stokes Simulations of Sonic Injection into Mach 2 Crossflow
・(AIAA2011-0734)Flow and Thermal Properties Induced by Electric Arc Plasma Actuators
・(AIAA2011-0662)DES Study of Base and Base-Bleed Flows with Dynamic Formulation of DES Constant
・(AIAA2011-0650)Simulations of High Speed Turbulent Jets in Crossflows
・(AIAA2011-0604)An Experimental Investigation of the Autoignition Characteristics of Camelina-Based Hydroprocessed Renewable Jet Fuel
・(AIAA2011-0567)Numerical Simulations of hypersonic boundary-layer instability with localized roughness
・(AIAA2011-0506)Analysis of Hydrogen Injection into the Combustor of HyShot-II Scramjet Engine Using ILES
・(AIAA2011-0504)Laser-Induced Plasma Ignition Experiments in a Scramjet Inlet
・(AIAA2011-0503)Effect of Thermally Induced Deformation in UVa Supersonic Combustion Facility
・(AIAA2011-0502)Conceptual Design of Short-Range Two-Stage Scramjet Vehicle
・(AIAA2011-0485)Flowfield Characteristics of Oblique Shocks Generated using Microjet Arrays
・(AIAA2011-0481)Experimental Investigations of a Hypersonic Shock Turbulent Boundary Layer Interaction
・(AIAA2011-0479)Modeling Structural Uncertainties in Reynolds-Averaged Computations of Shock/Boundary Layer Interactions
・(AIAA2011-0478)Multi-Scale Turbulence Model in Simulation of Supersonic Crossflow
・(AIAA2011-0405)Numerical Investigations of NOx-Formation in Scramjet Combustors using Wall and Strut Injectors
・(AIAA2011-0404)CFD Analysis of an Inlet-Isolator Combination for Dual Mode Scramjet Applications
・(AIAA2011-0402)Scramjet Isolator Shock Train Location Techniques
・(AIAA2011-0401)The role of the baroclinic term in supersonic fuel/air mixing enhancement
・(AIAA2011-0400)Modeling Hypersonic Propulsion Using Finite Element CFD
・(AIAA2011-0399)CFD Aided Development of an Experimental Setup to Investigate Internal Supersonic Combustion
・(AIAA2011-0387)Hot flow testing of dual bell nozzles
・(AIAA2011-0373)Instability of hypersonic boundary layer on a wall with resonating micro-cavities
・(AIAA2011-0333)Supersonic Combustion and Flame-Holding Characteristics of Pylon Injected Hydrogen in a Mach 2.4 High Enthalpy Flow
・(AIAA2011-0323)Large Eddy Simulation of Supersonic Combustion in a Cavity-Strut Flameholder
・(AIAA2011-0322)A multivariate quadrature based moment method for supersonic combustion modeling
・(AIAA2011-0321)Stratified Jet Flames in a Heated (1364 K) Cross-Flow with Auto-ignition
・(AIAA2011-0320)Development of a Model Scramjet Combustor
・(AIAA2011-0319)Ignition and Near-Wall Burning in Transverse Hydrogen Jets in Supersonic Crossflow
・(AIAA2011-0317)Extinction Limits of C1-C4 Hydrocarbon and Air Nonpremixed Flames Relevant for Hypersonic Applications
・(AIAA2011-0315)Autoignition, Flame Propagation, and Extinction of Binary Fuel Blends of n-Decane/Ethylene and n-Decane/Methane
・(AIAA2011-0309)Mixing Characteristics of Active Microjet-Based Actuators in a Supersonic Backward-Facing Step Flow
・(AIAA2011-0306)The Influence of Turbulence-Chemistry Interaction Modelling for Supersonic Combustion
・(AIAA2011-0250)Simulation of Radiating Flows in Impulsive Facilities
・(AIAA2011-0231)An ILES Analysis of Transverse Jet Injection in to Supersonic Cross-flow with Synthetic Turbulent Boundary Layer
・(AIAA2011-0208)Large-eddy simulation of supersonic, turbulent mixing layers downstream of a splitter plate
・(AIAA2011-0074)Application of Compound Compressible Flow to a Boundary Layer in a Hypersonic Three-Dimensional Inlet
・(AIAA2011-0073)Characterisation of Supersonic Combuster Inlet Flows Using Diode Laser Absorption Spectroscopy
・(AIAA2011-0068)Unstart of a Supersonic Model Inlet/Isolator Flow Induced by Mass Injection