Short range acoustic propagation through non-linear internal waves - - PowerPoint PPT Presentation

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Short range acoustic propagation through non-linear internal waves - - PowerPoint PPT Presentation

Short range acoustic propagation through non-linear internal waves Daniel Rouseff, DajunTang, Kevin L. Williams Applied Physics Laboratory, University of Washington James N. Moum Oregon State University Zhongkang Wang Hangzhou Applied


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Short range acoustic propagation through non-linear internal waves

Daniel Rouseff, DajunTang, Kevin L. Williams Applied Physics Laboratory, University of Washington James N. Moum Oregon State University Zhongkang Wang Hangzhou Applied Acoustics Research Institute

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Introduction

On August 18, mid-frequency acoustic transmission data were collected on a vertical array over a continuous 7-hour period at range 550 m. The combination of acoustic frequency (1 to 10 kHz) and range (550 m) were expected to be useful for studying the effects of both linear and non-linear internal waves

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Motivation

Linear internal waves often are modeled as a background random process introducing random fluctuations in the acoustic field.

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Linear internal waves often are modeled as a background random process introducing random fluctuations in the acoustic field.

(From Flatté et al. [1978].)

Acoustic fluctuations may be examined using WPRM theory:

Scattering Theory Regimes

Motivation

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Linear internal waves often are modeled as a background random process introducing random fluctuations in the acoustic field.

(From Flatté et al. [1978].)

Acoustic fluctuations may be examined using WPRM theory:

  • At 1 kHz and range 550 m, should be

in weak-scattering Rytov regime.

  • At 10 kHz and range 550m, should be

in strong-scattering regime.

Scattering Theory Regimes

Motivation

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Non-linear internal waves are often modeled as a more event-like process causing strong, localized changes in the acoustic sound speed.

Example: Isotachs observed during 1996 Coastal Mixing and Optics Experiment (from Rouseff, 2001).

Motivation

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Non-linear internal waves are often modeled as a more event-like process causing strong, localized changes in the acoustic sound speed. 550 m acoustic path might permit individual waves in the packet to be isolated.

Example: Isotachs observed during 1996 Coastal Mixing and Optics Experiment (from Rouseff, 2001).

Motivation

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Data Modeling and Analysis

Present analysis considers ~0.5 hours of data collected immediately before, during, and after the passage of a non-linear internal wave.

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Pre Non-Linear Internal Wave

Measured sound speed profiles showed anomalous bump at ~30 m that hadn’t been observed earlier in

  • experiment. Layer of warm, salty,

neutrally buoyant water present. Based on measurements, decision made to put source at depth 40 m. (Source depth was 30 m on data collected earlier in experiment.)

1490 1500 1510 1520 1530 10 20 30 40 50 60 70

13:45 UTC 14:38 UTC

sound speed (m/s) depth (m)

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Modeling Result: Eigenrays to receiver at depth 50 m for assumed range-independent environment. Indistinct direct path sensitive to details of sound speed profile. Strong, distinct bottom-bounce path. Experimental Result: Matched filter

  • utput for LFM chirp signal.

Strong, distinct bottom-bounce path.

Pre Non-Linear Internal Wave

3 6 3 6 5 3 7 3 7 5 3 8 3 8 5 3 9

  • 2 . 5
  • 2
  • 1 . 5
  • 1
  • 0 . 5

0 . 5 1 1 . 5 2 2 . 5 t i m e ( m s ) c h n = 5 S D B B S S B

bottom direct surface bottom- surface surface- bottom 360 370 380 390 m a t c h e d f i l e t e r

  • u

t p u t ( a r b ) arrival time (ms)

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Internal Wave “Sonny”

Non-linear internal wave named “Sonny” as observed by radar aboard the R/V Knorr. R/V Oceanus collected oceanographic data on Sonny in close proximity to acoustic source deployed off stern of R/V Knorr.

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Experiment Geometry

Positioning of Assets:

acoustic source acoustic receiver

  • ceanographic

measurements

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Internal Wave “Sonny”

Measurements made from R/V Oceanus

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Experiment Geometry

Positioning of Assets:

acoustic source acoustic receiver

  • ceanographic

measurements

Using the measured bearing and speed (0.89 m/s) of Sonny observed at R/V Oceanus, we can estimate when wave will pass acoustic assets.

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Experiment Geometry

acoustic source acoustic receiver

  • ceanographic

measurements Time 21:14:00

Using the measured bearing and speed (0.89 m/s) of Sonny observed at R/V Oceanus, we can estimate when wave will pass acoustic assets. Positioning of Assets:

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Experiment Geometry

Positioning of Assets:

acoustic source acoustic receiver

  • ceanographic

measurements Time 21:14:00

Using the measured bearing and speed (0.89 m/s) of Sonny observed at R/V Oceanus, we can estimate when wave will pass acoustic assets.

Time 21:18:30

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Experiment Geometry

Positioning of Assets:

acoustic source acoustic receiver

  • ceanographic

measurements Time 21:14:00

Using the measured bearing and speed (0.89 m/s) of Sonny observed at R/V Oceanus, we can estimate when wave will pass acoustic assets.

Time 21:18:30 Time 21:28:31

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Results

Acoustic arrival pattern evolving over 32 minutes at depth 50 m. Bulk shift in arrivals due to source and/or receiver motion. Bottom (B), Surface-Bottom (SB) and Bottom-Surface (BS) paths noted as is position of internal wave. Main Result: New acoustic path “splits” from bottom bounce as internal wave passes above acoustic source.

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Results

New acoustic arrival induced by passing internal wave arrives at steeper angle than original bottom-bounce path.

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Results

Hypothesis: Upward launched ray refracted downward by passing internal wave. Ray strikes bottom further downrange than original bottom-bounce path and so arrives at receiving array at steeper angle.

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Modeling

cup = 1530 m/s clow = 1495 m/s

Preisig and Duda (1997) developed a 3-layer model for the sound speed:

  • Upper layer cup, lower layer clow,

middle layer with constant gradient.

  • Soliton model for IW displacement:

Range-dependent sound speed

1530 m/s 1495 m/s

η(x,t) = asech2((x − cpt)/ L)

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Modeling

cup = 1530 m/s clow = 1495 m/s

Preisig and Duda (1997) developed a 3-layer model for the sound speed:

  • Upper layer cup, lower layer clow,

middle layer with constant gradient.

  • Soliton model for IW displacement:

Apply model in ray trace study to test hypothesis using appropriate parameter values: cup = 1530 m/s, clow = 1495 m/s, zup = 18 m, zlow = 30 m, a = 8 m, L = 100 m, cp = 0.89 m/s.

Range-dependent sound speed

1530 m/s 1495 m/s

η(x,t) = asech2((x − cpt)/ L)

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Modeling

Pre soliton rec 1530 m/s 1495 m/s

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Modeling

1530 m/s 1495 m/s rec

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Modeling

1530 m/s 1495 m/s rec

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Modeling

1530 m/s 1495 m/s rec

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Modeling

1530 m/s 1495 m/s rec

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Modeling

1530 m/s 1495 m/s rec

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Summary

Mid-frequency acoustic transmission data were collected on a vertical array over a continuous 7-hour period at range 550 m. Present analysis considers data collected immediately before, during, and after the passage of a non-linear internal wave. Results show a new acoustic path being generated as the internal wave passes above the acoustic source. Simple model produces results consistent with observed new ray path. Future work includes: acoustic data analysis of complete 7-hour period; range- dependent acoustic modeling that is better integrated with the collected

  • ceanographic data; data/model comparison; data/scattering-theory comparison.