Collen et al., 2021 - Google Patents
Development and commissioning of the T6 Stalker TunnelCollen et al., 2021
View HTML- Document ID
- 2850858107813632937
- Author
- Collen P
- Doherty L
- Subiah S
- Sopek T
- Jahn I
- Gildfind D
- Penty Geraets R
- Gollan R
- Hambidge C
- Morgan R
- McGilvray M
- Publication year
- Publication venue
- Experiments in Fluids
External Links
Snippet
Abstract The T6 Stalker Tunnel is a multi-mode, high-enthalpy, transient ground test facility. It is the first of its type in the UK. The facility combines the original free-piston driver from the T3 Shock Tunnel with modified barrels from the Oxford Gun Tunnel. Depending on test …
- 238000011161 development 0 title abstract description 21
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Collen et al. | Development and commissioning of the T6 Stalker Tunnel | |
| Mirels | Shock tube test time limitation due to turbulentwall boundary layer | |
| Reynier | Survey of high-enthalpy shock facilities in the perspective of radiation and chemical kinetics investigations | |
| Gildfind et al. | Production of high-Mach-number scramjet flow conditions in an expansion tube | |
| Lynch et al. | Design and characterization of the Sandia free-piston reflected shock tunnel | |
| Hannemann et al. | The high enthalpy shock tunnel Göttingen of the German aerospace center (DLR) | |
| McGilvray et al. | T6: The Oxford University Stalker Tunnel | |
| Hannemann et al. | Recent extensions to the high enthalpy shock tunnel Göttingen (HEG) | |
| Grossir | Longshot hypersonic wind tunnel flow characterization and boundary layer stability investigations | |
| Collen et al. | Commissioning of the t6 stalker tunnel | |
| Fahy | Superorbital re-entry shock layers: flight and laboratory comparisons | |
| Fomin et al. | Hypersonic short-duration facilities for aerodynamic research at ITAM, Russia | |
| Yuan et al. | Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics | |
| James et al. | Experimentally simulating giant planet entry in an expansion tube | |
| Morgan et al. | A review of the use of expansion tubes for creating superorbital flows | |
| Leibowitz et al. | Hypervelocity spherically-blunted cone flows in Mars entry ground testing | |
| Mundt | Development of the new piston-driven shock-tunnel HELM | |
| James et al. | Generating high-speed earth reentry test conditions in an expansion tube | |
| James et al. | Experimentally simulating gas giant entry in an expansion tube | |
| Chazot et al. | TPS ground testing in plasma wind tunnel for catalytic properties determination | |
| Andrianatos et al. | A study of radiation scaling of high enthalpy flows in expansion tubes | |
| Olivier et al. | Operation, capabilities and limitations of existing hypersonic facilities | |
| Stennett et al. | Large-scale free-piston-driven multi-mode shock expansion tunnel | |
| Shams et al. | Capability analysis of global hypersonic wind tunnel facilities for aerothermodynamic investigations | |
| McGilvray | Scramjet testing at high enthalpies in expansion tube facilities |