Award Year / Program / Phase:
2010 / STTR / Phase II
Agency / Branch:
DOD / NAVY
Research Institution:
Penn State University
The noise from turbulent, hot, supersonic jets during take-off and landing, as well as high-Mach cruise at altitude, dominates noise emanating from other powerplant components (e.g., fan, combustor). This intense noise has significant safety implications for launch personnel as well an environmental…
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