NASA NTRS · 19730003299
Sonic inlet development for turbofan engines
Abstract
The static program has shown to date that very large noise reductions can be achieved by the sonic inlet concept with realistic inlet length and good aerodynamic performance. It is also shown that different inlet concepts produce substantially different results.
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Klujber, F.. 1972-01-01. Sonic inlet development for turbofan engines. https://ntrs.nasa.gov/citations/19730003299
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