All Stories

  1. Inward turning base-bleed technique for base drag reduction
  2. Study on oil-cooler location for a pusher type turbo prop aircraft using numerical simulation
  3. Acoustic pressure oscillation effects on mean burning rates of plateau propellants
  4. Investigation of Slender Bodies at Hypersonic Mach Numbers
  5. Mean Burning Rate Variation in Composite Propellant Combustion Due to Longitudinal Acoustic Oscillations
  6. Conceptual Design, Material, and Structural Optimization of a Naval Fighter Nose Landing Gear for the Estimated Static Loads
  7. Supersonic jet flow control using semi-circular corrugated tabs
  8. Effects of Angle of Attack and Bluntness on Heating Rate Distribution of Blunt Models at Hypersonic Speeds
  9. Heat transfer rate and surface pressure measurements in short duration hypersonic flow
  10. Non-Gaussian Wind Pressure Characteristics of HAWT Tower System with and Without Rotor
  11. Visualization of Shock Wave Phenomenon around a Sharp Cone Model at Hypersonic Mach Number in a Shock Tunnel using High Speed Schlieren Facility
  12. Oscillatory Pressure Effect on Mean Burning Rates of Solid Propellant Combustion at Low Frequency Conditions
  13. Drag Reduction of Non-Circular Cylinder at Subcritical Reynolds Numbers
  14. Convective heat-transfer rate and surface pressure distribution over a cone model at hypersonic speeds
  15. Jet Flow Control Using Semi-Circular Corrugated Tab
  16. Wind Tunnel Investigation of Downstream Wake Characteristics on Circular Cylinder with Various Taper Ratios
  17. Investigation of Engine Oil-cooling Problem during Idle Conditions on Pusher Type Turbo Prop Aircraft
  18. Wall Pressure Measurements in a Convergent–Divergent Nozzle with Varying Inlet Asymmetry
  19. Effect of Boundary Layer Fence Location on HAWT Power Performance
  20. Effect of Pitch Angle on Blade - Tower Interference on HAWT
  21. Influence of Boundary Layer Control on Wind Turbine Blade Aerodynamic Characteristics - Part I - Computational Study