Finite Element Simulation of the Second Sound Wave in a Chamber Annulus Wall of a Rotating Detonation Engine.- Detonation Flame Arrestor Design and Performance Evaluation Using Experimental and Numerical Methods.- Streamline-Traced Inlet Design and Integration with Rotating Detonation Engines.- Numerical Investigation of a Scramjet Engine with Two Opposing Cavities.- Numerical Analysis of Scramjet Inlet and Isolator According to the Heat Transfer Boundary Condition.- Multi Wave Mode Analysis of Methane Oxygen Rotating Detonation.- Characteristics of Supercritical JetA injection in Supersonic Crossflow.- Wave Dynamics in a Small Scale Continuous Detonation Combustor.
- Shuttling Transverse Detonation Waves in a Linear Channel.- Hinge Line Suction for the Investigation of Streamwise Vortices in a Hypersonic Compression Corner Flow.- Unsteadiness of the Cavity Shear Layer at a Hypersonic Speed.- Magnetohydrodynamic experiments conducted in a detonation driven high enthalpy shock tunnel.- Experimental and Numerical Investigation on the Longitudinal Stage Separation for Parallel staged Two stage to orbit Vehicle.- Using supersonic flows for separating carbon dioxide from industrial gaseous effluents.- Effect of Magnetohydrodynamic Aerobraking on Flow Field Surrounding an Earth Re Entry Capsule.- Unstart Prediction of Scramjet Engine for Variable Mach Number.
- Shock Tube Study of HTPB Ignition Using an Endwall Injector.- Initial evolution of drop post weak shockwave interaction in the bag regime.- Unsteady Heating Experiments of Silicon-based Heat resistant Materials in High enthalpy Flows Simulating Earth''s Atmospheric Reentry Environments.- Experimental Investigation of RP 1 Ignition Delay Time at Low Pressure Conditions.- Experimental Study on Shock Wave Attenuation Phenomena by Multi layered Wire Gauze Interaction.- Design and Evaluation of Experimental Methods to Study Thermochemical Nonequilibrium in Expanding Flows using TDLAS.- Three Dimensional Computational Study over a Hyper Ballistic Missile body at different Hypersonic Mach Numbers.- Effects of Nozzle Pressure Ratio on Mixing Characteristics of Underexpanded Sonic Twin Jets.
- Numerical modeling of blast wave interaction with spatially disseminated burnable liquid simulant.- Vacuum Ultraviolet and Visible Spectral Measurements for Simulated Saturn Entry in the X2 Expansion Tube.- A Numerical Study of Propagation of Rotating Detonation Wave under Non Uniform Inflow Conditions.- Strategies for Supersonic Flow Control Using ns DBD Plasma Actuators.- Numerical Studies of Shuttling Transverse Combustion with Discrete Injection of Premixed Reactant Mixture.- Experimental Investigations on Shock Train Oscillations in an Isolator.- Decay of Shock Waves in Detonation Driven Shock Tubes.- Characterizing the Freestream of the Caltech Hypervelocity Expansion Tube Part I: Facility Gas Dynamics and Simulations.
- Characterizing the Freestream of the Caltech Hypervelocity Expansion Tube Part II: Diode Laser Measurements Targeting Atomic Potassium.- Preliminary results for CO 2 recombination for low velocity, high density Mars aerocapture conditions.- A Converging Shock Tube for Strong Shock Interface Interaction Investigation.- Self Excited Oscillation of Normal Shock Wave/Boundary Layer Interaction in Internal Flow.- Shock Train Dynamics in Nozzle Isolator Co-flow Configuration.- Comparison of Static Pressure Measurement Techniques in the T5 Free Piston Reflected Shock Tunnel.- Large Eddy Simulation of Transverse Injection of Hydrogen in A High Enthalpy Crossflow.- Free-piston Driver Performance at High Compression Ratios in the X2 Expansion Tube.
- Curved Body Integrated Diverterless Supersonic Intake (DSI) Design.- A Hybrid High Speed Schlieren and Laser Absorption Diagnostic for Underexpanded Supersonic Jets under Rapid Backpressure Variation.- Interferometric visualization of detonation waves propagating premixed fuel and oxidant jet train.- Effect of Tip Curvature on the Aerodynamic Performance of an Osculating Cone Waverider.- Effect of Premixed Jet Height on Propagation of Detonation Wave inside Linear Detonation Channel.- Analysis on Pressure Gain of Rotating Detonation Engine.- Experimental investigation of Magnetohydrodynamic Aerobraking for High Velocity Mars Entry.- Scaling of Upstream Influence Line Induced by Swept Shock Wave/Turbulent Boundary Layer Interactions on a Concave Half Cylinder.
- Backshell Radiative Heating and Shock Layer Kinetic Measurement in NASA''s Electric Arc Shock Tube Facility.- Numerical study on large amplitude oscillatory unstart in a 2D scramjet intake.- Comparison of experimental and numerical results of a methane oxygen rotating detonation engine.- Shock dynamics of sub critical detonation diffraction.- Optical Measurement Technique for Thermo acoustic Pressure Detection in a Combustion Chamber.- Modelling and experiments of the triple point reflection in detonations.- Rapid Scanning Tunable Laser Absorption Measurements of Shock Heated Nonequilibrium Air Species in the NASA Electric Arc Shock Tube.- Experimental Study of Tandem Cavity Scramjet Combustor Ignition using a micro Pulse Detonation Engine.
- Detonation attenuation and quenching in hydrogen mixtures after the interaction with cylinders.