NASA NTRS · 20100042199
Highly Variable Cycle Exhaust Model Test (HVC10)
Abstract
Results from acoustic and flow-field studies using the Highly Variable Cycle Exhaust (HVC) model were presented. The model consisted of a lobed mixer on the core stream, an elliptic nozzle on the fan stream, and an ejector. For baseline comparisons, the fan nozzle was replaced with a round nozzle and the ejector doors were removed from the model. Acoustic studies showed far-field noise levels were higher for the HVC model with the ejector than for the baseline configuration. Results from Particle Image Velocimetry (PIV) studies indicated that large flow separation regions occurred along the ejector doors, thus restricting flow through the ejector. Phased array measurements showed noise sources located near the ejector doors for operating conditions where tones were present in the acoustic spectra.
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Henderson, Brenda, Wernet, Mark, Podboy, Gary, Bozak, Rick. 2010-10-22. Highly Variable Cycle Exhaust Model Test (HVC10). https://ntrs.nasa.gov/citations/20100042199
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