The development of injector units for jet-lift engine simulation on low-speed-tunnel models

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dc.contributor.author M. N. Wood en_US
dc.contributor.author J. B. W. Howard en_US
dc.date.accessioned 2014-10-21T15:56:33Z
dc.date.available 2014-10-21T15:56:33Z
dc.date.issued 1965 en_US
dc.identifier.other ARC/R&M-3464 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4042
dc.description.abstract Small-scale injector units have been developed for providing the engine nacelles of V/STOL models, with both intake and exit flows. The primary energy supply was cold compressed air at pressure ratios up to 4:1. With the chosen injector arrangement, a stable and uniform exit velocity distribution was achieved, with a mean velocity of nearly 650 ft/sec, and almost 50 per cent of the jet efflux drawn in through the intake. The requirements for engine simulation on model scale, and the capabilities and limitations of injector units for this application are discussed in an Appendix. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title The development of injector units for jet-lift engine simulation on low-speed-tunnel models en_US


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