All Stories

  1. Experimental Investigation of Hypersonic Sharp-Fin Shock-Wave/Transitional-Boundary-Layer Interactions
  2. Shock Perturbations in Attached Turbulent Shock-Wave/Boundary-Layer Interactions at Mach 6
  3. The Aerodynamics of Free-Flying Cylinders in High Supersonic Flow
  4. An Experimental Investigation on the Effects of Dust on Separating Sphere Clusters in Hypersonic Flow
  5. Hypersonic Aerothermal Computations of a Sharp Fin Interaction
  6. Flow Characterization of a Newly Commissioned High-Temperature Ludwieg Tube at the University of Maryland
  7. Development of a Supersonic Ludwieg-Tube Facility for Investigating High-Speed Multi-Phase Flows
  8. High Enthalpy Effects on Hypersonic Boundary-Layer Transition: T5 Experimental and Numerical Comparison
  9. Computer-Graphics-Based Optical Tracking for Hypersonic Free-Flight Experiments
  10. Fluid-Thermal-Structural Interactions in Ramp-Induced Shock-Wave Boundary-Layer Interactions at Mach 6
  11. Development of a Direct-Connect Testing Capability in the HyperTERP Shock Tunnel
  12. Direct Numerical Simulation of Boundary Layer Receptivity to Acoustic Radiation in a Hypersonic Compression Ramp Flow
  13. Characterization of High-Frequency Acoustic Sources Using Laser Differential Interferometry
  14. Direct Simulation of Fluid–Structure Interaction in a Hypersonic Compression-Ramp Flow
  15. Hypersonic Fluid–Structure Interactions in Compression Corner Shock-Wave/Boundary-Layer Interaction
  16. Interaction of Hypersonic Boundary-Layer Instability Waves with Axisymmetric Compression and Expansion Corners
  17. A Roadmap for Obtaining and Implementing Heat Flux Measurements in the Hypersonic Environment
  18. Separation dynamics of a spherical particle detaching from a two-dimensional ramp in hypersonic flow
  19. Visualizations of Boundary-Layer Transition on a Sharp Cone at Mach 6
  20. Visualizations of Hypersonic Boundary-Layer Transition on a Variable Bluntness Cone
  21. HyperTERP: A newly commissioned hypersonic shock tunnel at the University of Maryland
  22. Particle tracer comparison in a Mach 3 Tunnel
  23. The impact of deformation on the aerodynamics of flapping dragonfly wings
  24. Unsteady Surface and Flowfield Measurements in Ramp-Induced Turbulent and Transitional Shock-Wave Boundary-Layer Interactions at Mach 6
  25. Theoretical and Numerical Study of a Preheated Ludwieg Tube with Adiabatic Compression
  26. Improved Analysis of the Lift Force on a Free-Flying Capsule in a Shock Tunnel
  27. Force and Moment Measurements on a Free-Flying Capsule in a Shock Tunnel
  28. Hypersonic Boundary-Layer Transition Features from High-Speed Schlieren Images
  29. Experimental study of second-mode instability growth and breakdown in a hypersonic boundary layer using high-speed schlieren visualization
  30. Adiabatic-compression preheated Ludwieg tube for the realistic simulation of hypersonic flows
  31. Free Flight Testing of a Scramjet Engine in a Large Scale Shock Tunnel
  32. Methods for Identifying Key Features in Schlieren Images from Hypersonic Boundary-Layer Instability Experiments
  33. Investigation of Hypersonic Boundary-Layer Transition Using High-Speed Visualization Techniques
  34. Fast-response temperature-sensitive-paint measurements on a hypersonic transition cone
  35. Schlieren-based techniques for investigating instability development and transition in a hypersonic boundary layer
  36. Visualization of Hypersonic Boundary-Layer Transition on a Slender Cone (Invited)
  37. Transient fluid-combustion phenomena in a model scramjet
  38. Dynamical separation of spherical bodies in supersonic flow
  39. Time-Resolved Visualization of Instability Waves in a Hypersonic Boundary Layer
  40. Shock-wave surfing
  41. An improved visualization-based force-measurement technique for short-duration hypersonic facilities
  42. Image-based force and moment measurement in hypersonic facilities
  43. Proximal bodies in hypersonic flow