- Presentation Archive -

11th International Workshop on Shock Tube Technology

(June 29, 2016, Germany)

• Agenda
  Text: pdf (79KB)
  
• Abstracts
  Text: pdf (3.53MB)
  
• Contents
1. On the history of free-piston shock tunnels up to the HEG
   Hans G. Hornung
   Text: pdf (10.9MB)
2. Hypersonic Research in the High Enthalpy Shock Tunnel Göttingen
   Klaus Hannemann
   Text: pdf (6.76MB)
3. Preliminary performance data for a Mach 12 scramjet operating condition in the X3 expansion tube
   Pierpaolo Toniato
   Text: pdf (16.0MB)
4. The Development of High Enthalpy Conditions for the X3 Expansion Tube Using the New Light-Weight Piston and Reservoir Extension
   Andreas Andrianatos
   Text: pdf (38.9MB)
5. Basic performance of the free-piston driven expansion tube JAXA HEK-X
   Hideyuki Tanno
   Text: pdf (2.27MB)
6. The Development of Hypersonic Pulse Facilities and Its Application at LHD
   Zhao Wei
   Text: pdf (2.16MB)
7. Scaling effects in shock tubes and tunnels
   Singh Tarandeep
   Text: pdf (4.04MB)
8. Reflected-Shock Experiments in Mixtures with Exotic Bath Gases
   Eric Petersen
   Text: pdf (2.96MB)
9. Recent Progress Towards High-Temperature Gas Dynamics in the Free-Piston Shock Tunnel HELM
   Claudio Selcan
   Text: pdf (1.87MB)
10. Influence of Thermal Sensors Installation on Measuring Precision at Stagnation Points
    Qiu Wang
    Text: pdf (1.59MB)
11. Novel Gauge to Measure Radiative Heat Transfer Rate on a Re-entry Body Flying at Hypersonic Mach Numbers Tested in Short Duration
    Srinath Sumo
    Text: pdf (1.94MB)
12. Development of a High Response Diamond Based Calorimeter Gauge
    Rowland Penty Geraets
    Text: pdf (3.94MB)
13. Analysis of upstream-moving pressure waves along a supercritical airfoil in a modified Shock Tube
    Bastian Hammer
    Text: pdf (1.47MB)
14. From Shock Tunnel to Flight and Back Again
    Allan Paull
    Text: pdf (7.79MB)
15. An Overview of Current Planetary Entry Research in the X2 Expansion Tube
    Christopher James
    Text: pdf (6.93MB)
16. Current research activities in JAXA-HIEST
    Hideyuki Tanno
    Text: pdf (4.12MB)
17. T6 Stalker Tunnel: Update on Progress
    Matthew McGilvray
    Text: pdf (9.56MB)
18. HYPULSE – A Versatile Hypersonic Research Facility
    Robert Bakos
    Text: pdf (4.75MB)
19. Two-Driver Shock Tubes: Configurations and Applications
    Akihiro Sasoh
    Text: pdf (2.38MB)
20. The X3R Reflected Shock Tunnel: Development of Long Duration Operating Conditions
    Samuel Stennett
    Text: pdf (5.31MB)
21. ISL Shock tunnel STA operation as Blowdown tunnel
    Berthold Sauerwein
    Text: pdf (2.06MB)
22. Boundary layer combustion experiments in the T4 Stalker Tube
    David J. Mee
    Text: pdf (2.22MB)
23. Experimental measurement of turbulent spot development behind multiple roughness elements in a transitional hypersonic boundary l
    Oliver Taylor
    Text: pdf (29.4MB)
24. Experimental study of instability growth and breakdown in a hypersonic
    Stuart Laurence
    Text: pdf (3.28MB)
25. High Frequency Free-Stream Disturbance Measurements in Hypersonic Wind Tunnels by Means of a Slender Wedge Probe
    Alexander Wagner
    Text: pdf (2.96MB)
26. In-pipe aerodynamic characteristics of a projectile in comparison with freeflight for transonic Mach numbers between 0.5 and 1.5
    Robert Hruschka
    Text: pdf (3.45MB)
27. Table Top, Hand-driven, Shock Tube and Hypersonic Shock Tunnel Facilities
    Ramesh Babu Rajamanickam
    Text: pdf (2.74MB)
28. Measurement of Aerodynamic Coefficients of Blunt Cones at the High Enthalpy Shock Tunnel Göttingen
    Damian Friedl
    Text: pdf (1.43MB)
29. Unsteady Injection behavior of Shock Vector Control
    Hilbert van Pelt
    Text: pdf (12.0MB)
30. Numerical Simulation of the Coupling of Aeroheating and Solid Heat Transfer for the Nozzle of the FL-63 High Enthalpy Wind Tunnel
    Zhansen Qian
    Text: pdf (1.95MB)
31. Analysis of Nonequilibrium Argon Plasmas based on a Collisional Radiative Model
    Gouji Yamada
    Text: pdf (0.98MB)
32. Emission Spectroscopy in a High Enthalpy Flow Facility
    Timothy McIntyre
    Text: pdf (7.93MB)
33. High Speed Emission Spectroscopy in HEG
    Troy Eichmann
    Text: pdf (2.85MB)
34. Study of Radiating Gas in a Shock Tube using a spectrometer
    Anbuselvan KKN (Tarandeep)
    Text: pdf (1.12MB)
35. Application of Temperature-Sensitive Paint Technique to Hypersonic Boundary Layer Transition in High Enthalpy Shock Tunnel
    Hiroki Nagai
    Text: pdf (12.8MB)
36. Highly Temperature Sensitive TSP Measurements on the Wall of Newly Built Shock-tube
    Hiroshi Ozawa
    Text: pdf (1.21MB)
37. Development of Ultra-fast Temperature Sensitive Paints for Hypersonic High Speed Flows
    Jan Martinez Schramm
    Text: pdf (19.5MB)
38. Closure
    Text: pdf (555KB)
39. [Movie] Beginning of HEG IWSTT 2016
    Zip: movie(wmv) (159MB)
40. [Photo] Group Photo
    Zip: jpeg (73.8MB)