NASA NTRS · 19710062902
Inlet-engine-nozzle wind tunnel test techniques
Abstract
Supersonic propulsion system inlet, engine and exhaust nozzle in wind tunnel and flight tests, discussing boundary layer effects on performance
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Bowditch, D. N.. 1971-09-01. Inlet-engine-nozzle wind tunnel test techniques. https://ntrs.nasa.gov/citations/19710062902
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