All Stories

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