All Stories

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