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Full Length Papers(Scramjet)(2010)

2010
AIR VEHICLES INTEGRATION AND TECHNOLOGY RESEARCH (AVIATR) Task Order 0015: Predictive Capability for Hypersonic Structural Response and Life Prediction, Phase 1 - Identification of Knowledge Gaps
Characterization of a High-Frequency Pulsed-Plasma Jet Actuator for Supersonic Flow Control
Modeling, Analysis, and Control of a Hypersonic Vehicle With Significant Aero-Thermo-Elastic-Propulsion Interactions, and Propulsive Uncertainty
Investigation of the shock wave/boundary layer interaction of scramjet intake flows
Multi-Objective Design Optimisation of Inlet and Combustor for Axisymmetric Scramjets
Physical Insight into Scramjet Inlet Behavior via Multi-Objective Design Optimization
Plasma assisted flame ignition of supersonic flows over a flat wall
Advances in LES of the HyShot II Scramjet Combustor
Direct numerical simulation of hypersonic turbulent boundary layers
Full-system RANS of the HyShot II scramjet Part 2: Reactive cases
Hydroxyl tagging velocimetry in a supersonic flow over a ramped-wall cavity flameholder with an upstream strut
Les modeling of combustion applications using OpenFOAM
Investigation of TDLAS Measurements in a Scramjet Engine
Permanent-Change Thermal Paints for Hypersonic Flight-Test
Versatile Affordable Advanced Fuels and Combustion Technologies
(AIAA2010-8708)Economic and Performance Analysis of Indian Space Transportation Systems
(AIAA2010-8281)LPV State feedback control for flexible hypersonic vehicle longitudinal dynamics
(AIAA2010-7930)Hypersonic Vehicle Flight Dynamics with Coupled Aerodynamics and Reduced-order Propulsive Models
(AIAA2010-7184)Evaluation of CFD Codes for Hypersonic Flow Modeling
(AIAA2010-7129)Design of a Catalytic Nitrous Oxide Decomposition Reactor
(AIAA2010-7128)Development and Testing of a High Temperature N2O Decomposition Catalyst
(AIAA2010-7125)Incorporation of a Trade Study Tool for Fuels Development within SRHEAT(TM)
(AIAA2010-7123)Scramjet engine combustor tests in a supersonic wind tunnel with a vitiated air heater
(AIAA2010-7066)Shock/Boundary Layer/Heat Release Interaction in the HyShot II Scramjet Combustor
(AIAA2010-7038)Research on combustion of hydrocarbon huel in a supersonic combustor
(AIAA2010-7036)Numerical Simulation of Auto-Ignition of Ethylene in a Scramjet Combustor with Air Throttling
(AIAA2010-6989)TDLAS-based Measurements of Temperature, Pressure, and Velocity in the Isolator of an Axisymmetric Scramjet
(AIAA2010-6962)An improved lobed strut injector concept for supersonic combustion
(AIAA2010-6957)Dual Mode Scramjet Design to Achieve Improved Operational Stability
(AIAA2010-6878)Flamelet/Progress-Variable Model for Large eddy Simulation of Supersonic Reacting Flow
(AIAA2010-6824)Extent and impacts of hydrocarbon fuel compositional variability for aerospace propulsion systems
(AIAA2010-6800)Nonlinear Liquid Rocket Combustion Instability Behavior Using UCDS Process
(AIAA2010-6794)Transpiration cooling with supersonic flows and foreign gas injection
(AIAA2010-6792)Large-eddy simulation of supersonic film cooling
(AIAA2010-6791)Continued Investigation of Short Contact Time Reactors for Regeneratively-Cooled Hypersonic Vehicles
(AIAA2010-6789)Optimization of Air-breathing Hypersonic Aircraft Design using Euler Codes and Genetic Algorithms
(AIAA2010-6787)Material Development (MatDev(TM)) Module for Use with SPIRITECH's Scramjet/Ramjet Heat Exchanger Analysis Tool (SRHEAT(TM))
(AIAA2010-6720)Experimental Study on Effect of Boundary Layer on Combustion Modes in a Supersonic Combustor
(AIAA2010-6646)Numerical Analysis of Fuel Injection Effects of the RBCC Engine in Ramjet Mode under Flight Mach 4 Condition
(AIAA2010-6644)Effect of a Vent Slot Mixer with a Plasma Jet Torch in Unheated Supersonic Flow
(AIAA2010-6642)Thermal management and fuel system model for TBCC dynamic simulation
(AIAA2010-6641)Hydraulic and Kinematic System Model for TBCC Dynamic Simulation
(AIAA2010-6557)High-Frequency Pressure Measurements for Unstart Detection in Scramjet Isolators
(AIAA2010-6556)CFD Modeling of an Isolator Shock Train in a Scramjet Engine
(AIAA2010-6554)Experimental Investigation of the Short Isolator with the Ramp under Asymmetric Incoming Flow
(AIAA2010-5009)Supersonic Cavity Flame Stabilization Studies using a Multivariate Quadrature based Moment Method
(AIAA2010-4999)High-speed boundary-layer transition induced by an isolated roughness element
(AIAA2010-4896)Modelling and Simulation of Heat Transfer on Functionally Graded Materials for Hot Structures in Scramjet Engines
(AIAA2010-4883)Hydroxyl Radical Kinetic Measurements in Low Temperature Nanosecond Pulsed Non-equilibrium Plasmas
(AIAA2010-4801)Testing of an Optically-Coupled Micro-Sensor for Wall Shear in Hypersonic Flow
(AIAA2010-4792)Development of the Scramjet Engine Test Facility in Korea Aerospace Research Institute
(AIAA2010-4761)Effects of plasma discharge on hypersonic flow over flat plate
(AIAA2010-4468)EXPERIMENTAL STUDIES OF SHOCK WAVE/TURBULENT BOUNDARY LAYER INTERACTION IN HIGH REYNOLDS NUMBER SUPERSONIC AND HYPERSONIC FLOWS TO EVALUATE THE PERFORMANCE OF CFD CODES
(AIAA2010-4454)Verification and Validation of Structured and Overset Grid Capabilities on Hypersonic Multibody Configurations
(AIAA2010-4320)Modeling Air-SiO2 Surface Catalysis under Hypersonic Conditions with ReaxFF Molecular Dynamics
(AIAA2010-4306)Performance Comparison between Hall and Diagonal Magnetohydrodynamic Generator with Circular Cross Section
(AIAA2010-4304)Study of Effects of Electrode Configuration of Full-Scale Scramjet Driven DCW MHD Generator with Three-Dimensional Analysis
(AIAA2010-4302)Comparison of generator performance of small-scale diagonal and Faraday MHD generators
(AIAA2010-4209)Focused schlieren and deflectometry at AEDC hypervelocity wind tunnel No. 9
(AIAA2010-4204)Miniature data-logger for aerodynamic force measurement in impulsive facility
(AIAA2010-3499)Using the Integrated Vehicle Health Management Research Test and Integration Plan Wiki to Identify Synergistic Test Opportunities
(AIAA2010-3007)Effect of Chemistry Modeling on Multidisciplinary Hypersonic Vehicle Design
(AIAA2010-1590)Kinetics of low-temperature hydrogen oxidation and ignition by repetitively pulsed nonequilibrium plasmas
(AIAA2010-1586)Mechanisms of Kinetic Combustion Enhancement by O2 (a 1Δg)
(AIAA2010-1574)Roughness-induced instability in a laminar boundary layer at Mach 6
(AIAA2010-1562)Numerical and Experimental Characterization of High Enthalpy Flow in an Expansion Tunnel Facility
(AIAA2010-1553)A WENO-Z based Eulerian-Lagrangian code for simulation of shocked flows laden with evaporating droplets.
(AIAA2010-1526)Supersonic Mixing Enhancement and Optimization Using Fin-Guided Fuel Injection
(AIAA2010-1512)Ignition and Oxidation of Ethylene-Air Mixtures at Elevated Pressures
(AIAA2010-1486)Facility for Shock and Detonation Wave Interaction with a Reactive Turbulent Field
(AIAA2010-1405)Hydroxyl tagging velocimetry in a supersonic flow over a piloted cavity
(AIAA2010-1400)Beam Shaping for CARS Measurements in Turbulent Environments
(AIAA2010-1344)Pulsed Thermionic Power Conversion with Positive Work Function Difference
(AIAA2010-1304)Advanced Capabilities for Wind Tunnel Testing in the 21st Century
(AIAA2010-1226)An Interactive Preliminary Design System of High Speed Forebody and Inlet Flows
(AIAA2010-1147)Numerical and experimental investigation of syngas combustion in a semitechnical scale burner
(AIAA2010-1127)Numerical simulation of vitiation effects on a hydrogen-fueled dual-mode scramjet
(AIAA2010-1122)Integrated Aero-Servo-Thermo-Propulso-Elasticity (ASTPE) Methodology for Hypersonic Scramjet Vehicle Design/Analysis
(AIAA2010-1098)Flow Control Using Thermal Bumps in Hypersonic Flow
(AIAA2010-1061)Hypersonic boundary-layer transition experiments in a Mach-6 quiet tunnel
(AIAA2010-0942)Parametric investigation of racetrack-to-circular cross-section transition of a dual-mode ramjet isolator
(AIAA2010-0856)Progress on a Rayleigh Scattering Mass Flux Measurement
(AIAA2010-0831)Velocity measurements in synthetic jet using magnetically driven surface discharges
(AIAA2010-0773)Predicting Mixing and Combustion in the Afterburn Stage of Air Blasts
(AIAA2010-0758)LES of the HyShot scramjet combustor
(AIAA2010-0757)Three-Dimensional Simulation of Ignition Transient in Hyshot Scramjet Configuration
(AIAA2010-0753)Supersonic Turbulent Mixing Structure in Staged Injection Flowfields
(AIAA2010-0651)Plasma enhanced combustion using microwave energy coupling in a re-entrant cavity applicator
(AIAA2010-0613)Impact of fischer-tropsch fuels on aero-engine combustion performance
(AIAA2010-0589)Experimental and Computational Investigation of a Dynamic Starting Method for Supersonic/Hypersonic Inlets
(AIAA2010-0588)Development of a Ludwieg tube with free piston compression heating for scramjet inlet starting experiments
(AIAA2010-0414)Large-Eddy Simulation of Cavity Flame-Holding in a Mach 2.5 Cross Flow
(AIAA2010-0384)Fabri choking in a two-dimensional reacting flow mixer-ejector
(AIAA2010-0379)Studies of Diamond-Shaped Injectors in a Supersonic Flow (Invited Presentation)
(AIAA2010-0370)LES/RANS simulation of a supersonic reacting wall jet
(AIAA2010-0310)Measurement of hypersonic high-enthalpy boundary layer transition on a 7o cone model
(AIAA2010-0302)Accuracy, Precision, and Scatter in TDLAS Measurements
(AIAA2010-0277)Near Stall Flow Analysis in the Transonic Fan of the RTA Propulsion System
(AIAA2010-0263)Plasma Assisted Flame Holding in Subsonic and Supersonic Flows
(AIAA2010-0259)High-Power Filamentary Pulse Discharge in Supersonic Flow
(AIAA2010-0232)The Effect of MHD Energy Bypass on Specific Thrust for a Supersonic Turbojet Engine
(AIAA2010-0212)Parametric study of primary breakup of turbulent liquid jets in crossflow: Role of Weber number
(AIAA2010-0203)Large eddy simulation of supersonic combustion using direct quadrature method of moments
(AIAA2010-0194)Spray structure of aerated liquid jets using double-view digital holography
(AIAA2010-0147)Effects of a Catalyst Coating on a PDE Endothermic Fuel Heating System
(AIAA2010-0143)Langley Ground Facilities and Testing in the 21st Century
(AIAA2010-0128)Error Estimation for High Speed Flows Using Continuous and Discrete Adjoints
(AIAA2010-0044)Direct measurement of skin friction in complex flows
(AIAA2010-0031)A Modular Conjugate Heat Transfer Capability for the Wind-US CFD Code
(AIAA2010-0027)An overview of the NPARC alliance's Wind-US flow solver