Author

W. H. Brown

Observed names: Brown, W. H., W. BROWN, W.H. Brown

Institution: General Electric (United States)

Observed institutions: Lockheed Martin (United States), Georgia Institute of Technology, General Electric (United States), Lockheed (United States)

OpenAlex ID: A5110141468

Coherent large-scale structures in high Reynolds number supersonic jets

1987 · J. Lepicovsky, K. K. Ahuja, et al. · AIAA Journal · 56

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Analysis of Thermal Stratification of Liquid Hydrogen in Rocket Propellant Tanks

1964 · J. W. Tatom, W. H. Brown, et al. · Springer eBooks · 50

Effects of nozzle exit boundary-layer conditions on excitability of heated free jets

1989 · J. Lepicovsky, W. H. Brown · AIAA Journal · 37

Acoustic control of free jet mixing

1986 · J. Lepicovsky, K. K. Ahuja, et al. · Journal of Propulsion and Power · 30

Noise from a circulation control wing with upper surface blowing

1987 · M. Salikuddin, W. H. Brown, et al. · Journal of Aircraft · 23

Shock associated noise of inverted-profile coannular jets, part I: Experiments

1985 · H.K. Tanna, W.H. Brown, et al. · Journal of Sound and Vibration · 22

Non-linear effects in finite amplitude wave propagation through orifice plate and perforated plate terminations

1990 · M. Salikuddin, W.H. Brown · Journal of Sound and Vibration · 16

Computational aeroacoustics as applied to the diffraction of sound by cylindrical bodies

1987 · M. M. S. Khan, W. H. Brown, et al. · AIAA Journal · 12

Non-linear effects in finite amplitude wave propagation through ducts and nozzles

1986 · M. Salikuddin, W.H. Brown · Journal of Sound and Vibration · 12

An improved impulse method for studies of acoustic transmission in flow ducts with use of signal synthesis and averaging of acoustic pulses

1984 · M. Salikuddin, K.K. Ahuja, et al. · Journal of Sound and Vibration · 11

Refinement and application of acoustic impulse technique to study nozzle transmission characteristics

1983 · M. Salikuddin, W. H. Brown, et al. · 9

Design and characterization of a high temperature and high frequencyinfinite-line pressure probe

1989 · M. SALIKUDDIN, R. BURRIN, et al. · 8

Enhancement of mixing in a rectangular jet by mechanical tabs

1990 · W. H. Brown, K. K. Ahuja · NASA STI Repository (National Aeronautics and Space Administration) · 6

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Acoustically excited heated jets. 1: Internal excitation

1988 · J. Lepicovsky, K. K. Ahuja, et al. · NASA Technical Reports Server (NASA) · 6

Acoustically excited heated jets. 3: Mean flow data

1988 · J. Lepicovsky, K. K. Ahuja, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 3

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Noise characteristics of upper surface blown configurations. Experimental program and results

1977 · W. H. Brown, N. Searle, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 3

Jet mixing enhancement by hydrodynamic excitation

1993 · W. H. Brown, K. K. Ahuja · AIAA Journal · 2

Acoustically excited heated jets. 2: In search of a better understanding

1988 · J. Lepicovsky, K. K. Ahuja, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 2

Shear flow control of cold and heated rectangular jets by mechanical tabs. Volume 1: Results and discussion

1989 · W. H. Brown, K. K. Ahuja · NASA STI Repository (National Aeronautics and Space Administration) · 1

Shear flow control of cold and heated rectangular jets by mechanical tabs. Volume 2: Tabulated data

1989 · W. H. Brown, K. K. Ahuja · NASA STI Repository (National Aeronautics and Space Administration)

Reduced Aircraft-Engine Noise

1983 · H.K. Tanna, W. H. Brown, et al. · NASA Tech Briefs

Shock associated noise reduction from inverted-velocity-profile coannular jets

1981 · H.K. Tanna, Christopher K. W. Tam, et al. · Lockheed Missiles and Space Co. Report

USB flow characteristics related to noise generation

1976 · W. H. Brown, N. N. Reddy · NASA Technical Reports Server (NASA)

Works count: 27

Citation count: 309

H-index: 10

I10-index: 10