dc.contributor.author | R. A. East | en_US |
dc.contributor.author | A. Qasrawl | en_US |
dc.date.accessioned | 2014-10-21T15:51:42Z | |
dc.date.available | 2014-10-21T15:51:42Z | |
dc.date.issued | 1978 | en_US |
dc.identifier.other | ARC/R&M-3844 | en_US |
dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/3128 | |
dc.description.abstract | The application of a long stroke isentropic free piston compressor as the energy source for an intermittent M = 6.85 hypersonic wind tunnel is described. The advantages of comparatively long running times of up to 0.5 s and uniform reservoir conditions at up to 90 bar and 600 K are discussed. Particular problems arising from the long stroke compression associated with both viscous flow effects and non-steady wave propagation are discussed and solutions suggested. The theoretical operating principles of long stroke compression tubes are presented and experimental results are given for a pilot facility with com- pression tube diameter of 0.032 m and length to diameter ratio of 120 and for a full scale facility with corresponding values of 0.11 m and 114. | en_US |
dc.relation.ispartofseries | Aeronautical Research Council Reports & Memoranda | en_US |
dc.title | Long stroke isentropic free piston hypersonic wind tunnel | en_US |