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Acoustic and laser doppler anemometer results for confluent and 12-lobed Ep3s mixer exhaust systems

[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002] 2002

Acoustic test and analysis of a counterrotating prop-fan model

Magliozzi, B.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989] 1989

Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight

Yamamoto, K., author.
Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, February, 1984. 1984-

Far-field acoustic power level and performance analyses of F31/A31 open rotor model at simulated sca

Sree, Dave, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2015. 2015-

Free-jet feasibility study of a thermal acoustic shield concept for AST/VCE application dual stream

Janardan, B. A.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1984] 1984

Modifications to the 4 x 7 meter tunnel for acoustic research engineering feasibility study.

Orlando, Fla. : DSMA Engineering Corporation; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986] 1986

Near-field acoustic power level analysis of F31/A31 open rotor model at simulated cruise conditions,

Sree, Dave, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2015. 2015-