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1
New aspects of subsonic aerodynamic noise theory /
Published 1973CONNECT
Government Document Electronic eBook -
2
Emission of sound from axisymmetric turbulence convected by a mean flow with application to jet noise /
Published 1972CONNECT
Government Document Electronic eBook -
3
Wind-tunnel measurements of surface-pressure fluctuations at Mach numbers of 1.6, 2.0, and 2.5 using 12 different transducers /
Published 1972CONNECT
Government Document Electronic eBook -
4
Emission of sound from turbulence convected by a parallel flow in the presence of solid boundaries /
Published 1973CONNECT
Government Document Electronic eBook -
5
Annoyance caused by aircraft en route noise /
Published 1992CONNECT
Government Document Electronic eBook -
6
Noise tests on an externally blown flap with the engine in front of the wing /
Published 1973CONNECT
Government Document Electronic eBook -
7
Aeroacoustics of low mach number flows fundamentals, analysis, and measurement /
Published 2023CONNECT
Electronic eBook -
8
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9
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10
Predicting the inflow distortion tone noise of the NASA Glenn Advanced Noise Control Fan with a combined quadrupole-dipole model /
Published 2012CONNECT
Government Document Electronic Conference Proceeding eBook -
11
Tone noise predictions for a spacecraft cabin ventilation fan ingesting distorted inflow and the challenges of validation /
Published 2012CONNECT
Government Document Electronic Conference Proceeding eBook -
12
An empirical temperature variance source model in heated jets /
Published 2012CONNECT
Government Document Electronic eBook -
13
Acoustic measurements of an uninstalled spacecraft cabin ventilation fan prototype /
Published 2012CONNECT
Government Document Electronic Conference Proceeding eBook -
14
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15
Preliminary aerodynamic investigation of fan rotor blade morphing /
Published 2012CONNECT
Government Document Electronic eBook -
16
Acoustic investigation of jet mixing noise in dual stream nozzles /
Published 2012CONNECT
Government Document Electronic eBook -
17
The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor /
Published 2013CONNECT
Government Document Electronic eBook -
18
Jet-surface interaction test : phased array noise source localization results /
Published 2013CONNECT
Government Document Electronic eBook -
19
The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator /
Published 2013CONNECT
Government Document Electronic eBook -
20
Near-field acoustic power level analysis of F31/A31 open rotor model at simulated cruise conditions, technical report II /
Published 2015CONNECT
Government Document Electronic eBook