アップした時点では
GoogleまたはGoogle Scholarで全文にアクセス可能でした。
Full Length Papers(Scramjet)(2020)
2020・Performance parameters analysis of an organic Rankine cycle for power generation from the heat of cooling scramjet
・Higher Order Simulation of Unstart in a Scramjet Model
・Effect of Shock-induced Flow Separation in Scramjet Intake at Flight Conditions
・Effect of wavy wall strut fuel injector on shock wave development and mixing enhancement of fuel and air for a scramjet combustor
・ENC-2020-0547 ACADEMIC SCRAMJET DESIGN TO FLIGHT AT 20 KM OF ALTITUDE AT MACH NUMBER 5.79 INTEGRATED AT ROCKET ENGINE S30
・ENC-2020-0046 CFD INVESTIGATION OF A SUPERSONIC COMBUSTION CHAMBER OF A SCRAMJET ENGINE
・ENC-2020-0045 THREE-DIMENSIONAL NUMERICAL INVESTIGATION OF A SCRAMJET INLET CONSIDERING MACH NUMBER VARIATION
・Reduced Order Chemical Kinetic Modeling for a Hydrogen Fueled Radical Farming Scramjet
・Scramjet Combustor Mixing Enhancement by Corrugated Strips for Non Reactive Jets-A Computational Approach
・Multivariable control of regeneratively-cooled scramjet engine with two-stage kerosene injection based on H∞ method
・Numerical Study of Shock Train in the Isolator of Scramjet Engine
・Combustion Characteristics of a Cavity Flameholder with a Burned-Gas Injector at the Cavity Bottom Wall in a Scramjet Model Combustor
・Effects of oxygen enrichment on supersonic combustion in a Mach 10 scramjet combustor
・Modeling and analysis of regenerative cooling channels for scramjet engine
・Study and Design of Hypersonic Scramjet Engine Inlet
・Numerical Investigation of the Shock Train in a Scramjet with the Effects of Back-Pressure and Divergent Angles
・Experimental and numerical heat transfer from vortex-injection interaction in scramjet flowfields
・Numerical Investigation of Variation of Combustion Efficiency of Scramjet Combustor with Change in Length of Wedge Shaped Strut Blunt End
・Numerical Analysis of Thermochemical Nonequilibrium Flows in a Model Scramjet Engine
・Test Complex M11: Research on Future Orbital Propulsion Systems and Scramjet Engines
・Ideal performance analysis of the scramjet with Pre-jet fuel