All Stories

  1. Retraction: “Universal benchmark data of the three-dimensional boundary layer blockage and average friction coefficient for in silico code verification” [Phys. Fluids 34, 041301 (2022)]
  2. Advancing Magnetohydrodynamic Propulsion for Sustainable and Efficient Space Exploration
  3. Microbubble Nucleation and Acoustic Softening Trigger Multiphase Sanal Flow Choking and Shock Waves in Liquid Rockets
  4. In Vitro Microbubble Nucleation and Sanal Flow Choking Induced Combustion Instabilities in Liquid Rocket Propulsion
  5. Enhancing Scramjet Combustion: Leveraging Shockwave-Fuel Interactions for Improved Mixing
  6. In Silico Study of Obstruction-Induced Spray Modulation in Injector Nozzles for Enhanced Atomization
  7. Experimental Validation of Dual-Head Electromagnetic Propulsion Through Rack and Pinion Integration
  8. In-Silico Analysis of Acoustic Wave Backpropagation Through Nozzle Boundary Layers of Rocket Motors at Liftoff
  9. In Silico Evaluation of Sonic Ring Standoff and Trailing Edge Expansion on Hypersonic Waverider Performance
  10. Unraveling Microbubble Nucleation and Sanal Flow Choking in Dual-thrust Hybrid Rockets: The Sonic Mach Equation Determines DDT Threshold
  11. Enhancing Rocket Control with Pintle Nozzles
  12. Curved Strut Wall Effects in Scramjet Combustion
  13. Continuous Electromagnetic Push-Pull Propulsion
  14. Enhancing Scramjet Combustor Efficiency Through Strut-Based Multi-Point Fuel Injection: In silico Analysis Utilizing the SST k-ω Model
  15. A Design Trade-Off of Mixture Ratio of Liquid Rocket Engine
  16. Optimizing High-Performance Dual-Thrust Hybrid Rocket Systems in Vacuum: Mitigating Sanal Flow Choking by Spraying High Heat Capacity Nano-Granules
  17. Angled Fuel Injection and Strut Design in Scramjets
  18. The Coanda Effect Unveiled: Compressible and Viscous Flow Dynamics in Aerodynamics and Coaxial Jet Mixing
  19. A Novel Gas Injection Blending Technique to Mitigate the Aerodynamic Heating in High-Speed Flows
  20. Increasing Sonic Ring Standoff Distance Reduces Aerodynamic Heating With High Heat Capacity Fluid Injection
  21. Revolutionizing Aircraft Oversight: A Unified Method to Technical Surveillance and Auditing for Global Aviation Regulatory Authorities
  22. In Silico Studies of the Upturned Wing Tip Aerodynamics for the Design Optimization of Multiple Winglets With Variable Cant Angles for Transonic Aircraft
  23. Investigation of Area Ratios in Convergent-Divergent Streamlines for Assessing Transonic Aerodynamic Performance Across Varied AoA in Different Airfoils
  24. In Silico Design of Detonation-Free High-Performance Dual-Thrust Solid and Hybrid Propellant Rockets Through the Application of the Chapman–Jouguet Condition
  25. Design Optimization of a Waverider to Enhance the Aerodynamic Efficiency
  26. State of the Art Digital Accountable and Customizable Aircraft Transit Inspection/Line Maintenance Toolbox for Enhancing the Aircraft Safety
  27. Erratum: “A closed-form analytical model for predicting 3D boundary layer displacement thickness for the validation of viscous flow solvers” [AIP Adv. 8, 025315 (2018)]
  28. How air bubbles in blood can choke arteries and trigger shock waves in heart and brain vessels
  29. Benchmark Data to Predict Flow Blockage and Friction in Pipes for Accurate Fluid Simulations
  30. The Effects of Ground Clearance and Boundary Layer Blockage Factor on the Aerodynamics Performance of the Hyperloop Pod and Transonic Ground-Effect Aircraft
  31. How ground proximity causes flow choking and shock waves under fast-moving aircraft
  32. Nanoscale Flow Choking and Spaceflight Effects on Cardiovascular Risk of Astronauts – A New Perspective
  33. Deflagration to Detonation Transition in Chemical Rockets with Sudden Expansion/Divergence Regions
  34. Design Optimization of Dump Diffusers with NACA 66-021 Shaped Flame Tube
  35. Genome Approach and Data Science Methods for Accelerated Discovery of New Solid Propellants with Desired Properties
  36. The Application of Energetic Materials Genome Approach for Development of the Solid Propellants Through the Space Debris Recycling at the Space Platform
  37. Conceptual Design and Contour Optimization of Altitude Compensation Nozzles for SSTO Vehicles
  38. Design of Pre-diffuser Cone for Dump Diffusers for Aero Gas Turbine Engines
  39. Studies on Flame Spread Acceleration and Detonation Kernel in a Dual-thrust Rocket
  40. A Conceptual Method to Recycle Space Debris into Fuels and Artificial Soil in the ISS for Numerous Applications
  41. Experimental and Numerical Studies on Jet Acoustic Characteristics of Chevron Nozzles
  42. External Flow Choking at the Landing Phase of Aircraft and Re-entry Vehicles
  43. electromagnetic piston engine
  44. Development of the Multifactorial Computational Models of the Solid Propellants Combustion by Means of Data Science Methods –Phase III
  45. Design of an Uninterrupted Propulsion System for Spinning Planet Landers for Soft Landing
  46. Modeling of Sanal Flow Choking Condition and Design Optimization of High Performance Dual-thrust SRMs
  47. Prediction of 3D Boundary Layer Blockage and the Grain Design Optimization of HVT Dual-thrust Hybrid Rockets
  48. Studies on 2D and 3D Boundary layer Blockage and External Flow Choking at Moving Wing in Ground Effect
  49. Boundary layer Blockage, Venturi Effect and Cavitation Causing Aerodynamic Choking and Shock Waves in Human Artery Leading to Hemorrhage and Massive Heart Attack – A New Perspective
  50. A Closed-form Analytical Model for Predicting 2D Boundary layer thickness for Verification, Calibration and Validation of Navier-Stokes Solvers
  51. Mechanical Characterization of a Thick-Walled Viscoelastic Hollow Cylinder under Multiaxial Stress Conditions
  52. RETRACTED: A closed-form analytical model for predicting 3D boundary layer displacement thickness for the validation of viscous flow solvers
  53. Dual-head Electromagnetic Variable Sweeping Speed Space Broom for Space Debris Mitigation
  54. Parametrical Optimization of a three-dimensional Dump Diffuser with Aerodynamically-shaped Flame Tube for Modern Aircraft Engines
  55. Design of Environmental Friendly Chevron Nozzles for Lower Stage Rockets
  56. Design Optimization and Performance Evaluation of A Monopropellant Satellite Thruster
  57. Studies on Boundarylayer Blockage and External Flow Choking at Moving Wing in Ground Effect
  58. Diagnostic Investigation of Nozzle Flow Choking Time and Stage Separation Sequence of a Multi-stage Rocket
  59. Thrust Vectoring
  60. Performance Evaluation of Aerospike Nozzles for Lucrative Thrust Vector Control
  61. 3D Flame Spread and Starting Transient in Dual-thrust Solid Propellant Rocket Motors
  62. Statistical Studies on Space Launches and the need for Active Debris Removal System
  63. Three-dimensional Jet Acoustic Characterization and Geometry Optimization of Chevron Nozzles
  64. 3D Flow Visualization and Geometry Optimization of Cavity based Scramjet Combustors using k-ω Model
  65. Influence of Starting Chamber Dynamics on Nozzle Flow Choking Time and the Liftoff Time of Dual-thrust Rockets
  66. Diagnostic Investigation of Flame Spread Mechanism in Dual-thrust Solid Propellant Rocket Motors
  67. Conceptual Design and Testing of a Dual-thrust Dual-head Electromagnetic Space Exploration Probe
  68. Numerical Simulation of Biology-Inspired Beetle Wings at Various Flying Conditions
  69. Phenomenological Introduction of Propulsion Aspect of External Flow Choking at Wing in Ground Effect
  70. 3D Flow Simulation of Dual Thrust Solid Rocket Motors during Starting Transient
  71. Diagnostic Investigation of Flow field Characteristics of Cavity based Scramjet Combustors
  72. Studies on Gravity Influence on Solid Propellant Burn Rate
  73. Studies on Ignition Delay and Flame Spread in High-Performance Solid Rocket Motors
  74. Studies on Aerodynamic Characteristics of Dump Diffusers for Modern Aircraft Engines
  75. Ignition Transient of Dual-Thrust Solid Propellant Rocket Motors - A Review
  76. An Attempt to Correlate Collision Theory with Aerodynamic Lift
  77. Chemical Rocket Propulsion
  78. Studies on Fluidic Injection Thrust Vectoring in Aerospike Nozzles
  79. Studies on Space Debris Tracking and Elimination
  80. Studies on Internal Ballistics of Dual-thrust Motors for Nozzleless Propulsion
  81. Aerodynamic Sound Reduction for Silent Aircraft
  82. Numerical Simulation of Transient Flows in Inert Simulators of Solid Rocket Motors
  83. Power Generation for Manned Space Mission
  84. Evaluation of Dynamic Burn Rate from the Extinction Compliance of Solid Rocket Motors
  85. Studies on Internal Flow Choking in Dual-Thrust Motors
  86. Starting Transient Flow Phenomena in Inert Simulators of Solid Rocket Motors with Divergent Ports
  87. Studies on Flow Characteristics of Variable Ejector Systems
  88. Diagnostic Investigation of Dump Gap Effects on Flow Features of Dump Diffusers
  89. Fluid-Throat-Induced Shock Waves During the Ignition Transient of Solid Rockets
  90. Insulation Qualification Studies for Cryogenic Rockets
  91. Studies on Ejector Systems for Hydrogen Fuel Cell
  92. A Phenomenological Introduction of Fluid-Throat in High-Velocity Transient Motors
  93. A Classical Evaluation of the Thermophysical Properties of Insulators for Cryogenic Rockets
  94. Diagnostic Investigation of Instabilities and Pressure Oscillations in High-Performance Solid Rockets
  95. Characterization of Dump Diffusers using a k-e Turbulence Model
  96. Thermoviscoelastic Characterization of a Composite Solid Propellant Using Tubular Test
  97. Flame Spread with Sudden Expansions of Ports of Solid Propellant Rockets