NASA NTRS · 19700014098
Single stage experimental evaluation of variable geometry inlet guide vanes and stator blading, part 6 Final report
Abstract
Variable geometry inlet guide vanes and stators for extending stable operation of supersonic cruise turbine engine compressor front stage
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Jones, B. A.. 1970-03-15. Single stage experimental evaluation of variable geometry inlet guide vanes and stator blading, part 6 Final report. https://ntrs.nasa.gov/citations/19700014098
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