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Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

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Page 1: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Lagrangian Models

Anne Douglass

Code 613.3 Atmospheric Chemistry and Dynamics Branch

NASA Goddard Space Flight Center

Page 2: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Lagrangian Models

Web of Science Search1994 - presentJournal of Geophysical Research AtmospheresGeophysical Research Letters

“trajectory” - title, key word, abstract - ~500 publications

Two main types of applications• Type 1

– Requires specific knowledge of air parcel origin

• Solar history

• Temperature history

– Valid for 5-7 days (some cases a few days longer)

• Type 2– Study “overall transport

properties”• Strat/trop exchange

• Tropical isolation

– Requires large numbers of parcels and statistical analysis of their behavior

Page 3: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

• Parcels have no inertia (m = 0), D = “Drag”,Vw = wind

• Parcels have no size yet “represent” their surroundings• Parcels don’t know about each other except when some

kind of explicit mixing is included

Assumptions about Trajectory Transport

md2x parcel

dt 2= D(Vw −

dxParcel

dt)

Page 4: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Trajectory Model Formulations• Kinematic Trajectory Models - use “w” field from 3D GCM or assimilation

– Advantages• Consistent with CTM model transport• Can resolve mesoscale convective motions and cloud transport if

3D model can.– Disadvantages

• Inadequate time resolution of adiabatic motion can lead to enhanced diabatic drift

• Isentropic/Diabatic Trajectory Models– Advantages

• Conservation of entropy - adiabatic motions removed• Diabatic motion usually more accurate than vertical motion field

since motion dependent on T not “w”– Disadvantages

• What is the best way to treat surface interaction, convection and moist processes?

Page 5: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

The “constant acceleration” solution

Neglects higher order terms in the Taylor series expansion of the first equation (source of truncation errors).

OTHER things to think about• time resolution of wind fields• interpolation errors• vertical wind issues• wind field errors• tropospheric process errors

Stohl A., Computation, Accuracy and Applications of Trajectories - A Review and Bibliography, Atmospheric Environment, 32, 947-966, 1998.

ErrorsThere are different approaches to solving the trajectory equation:

X1(t1) ≈ X(t0) +1

2(Δt)[X(t0) + X(t1)]

dX

dt= ˙ X [X(t)]

Page 6: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Types of applications:

• interpretation of aircraft and satellite constituent observations

• trajectory mapping for satellite validationMorris et al., Trajectory mapping: A tool for validation of trace gas

observations, J. Geophys. Res., 105, 17,875-17,894, 2000.

Danilin, M. Y., Comparison of ER-2 aircraft and POAM III, MLS, and SAGE II satellite measurements during SOLVE using traditional correlative analysis and “trajectory hunting technique”, J. Geophys. Res., 107, doi:10.1029/2001JD000781, 2002.

• overall transport properties

Page 7: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Interpretation of stratospheric constituent observations

1. Assume you can come up with a solution to initialization issues for constituents that change on time scales of the integration e.g., NOx/Noy

2. Use the trajectories to account for solar history photolysis rates

overhead O3 columncloudsreflectivity

Keep some sense of how errors related to mixing or position errors in the trajectories can impact results.

Page 8: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Pierson, J. M. et al., Influence of air mass histories on radical species during the Photochemistry of Ozone Loss in the Arctic Region in Summer (POLARIS) mission, J. Geophys. Res., 105, 15,185-15,199, 2000.

APPLICATION 1 - Use back trajectories + photochemical model to interpret stratospheric aircraft observations

NASA’s ER-2 was deployed for the Photochemistry of Ozone Loss in the Arctic Region in Summer (POLARIS) mission flown during the summer of 1997 to measure radicals responsible for the summer photochemical destruction of ozone.

One key aspect of this decline is the concentration of nitrogen radicals, and their abundance relative to the reservoir HNO3.

Page 9: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Parcel Theta (K) 0 349.0 6 493.0 10 502.0 14 502.0 18 507.0 22 504.0 26 500.0 30 481.0

10-Day Back Trajectories for 970426

3030

00

2626

2626

1414

High latitude summer is nearly continuously in sunlight, but back trajectories show that late April air parcels intercepted by the ER-2 have different solar history.

2222

Page 10: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

There are chemical differences (apparent in both plots).

The outliers (from the late April flight shown on the previous slide) join the main group when the solar history is accounted for using back trajectories.

Subsequent laboratory measurements of the rates for

NO2 + OH + M HNO3 + Mand

OH + HNO3 NO3 + H2Ogreatly reduce the model - measurement disparity.

NOx/Noy measured

April 26 points are outliers

NOx/Noy measured

NO

x/N

oy m

odel

edN

Ox/

Noy

mod

eled

Page 11: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

IssuesInitializationNOx/NOy was initialized in for both calculations using

observations at the flight track. The steady state calculation produces higher NOx/NOy because periods of darkness and latitudinal variation of solar zenith angle are not accounted for.

MixingThis calculation assumes no mixing.

Trajectory errorsAlthough 10 days is a long time for a backward trajectory,

the solar history is likely to have smaller errors than the exact location, and this is the main source of error for the steady-state comparison.

(and trajectories are more serene in a summer circulation . . .)

Page 12: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

APPLICATION 2 - REVERSE DOMAIN FILL

If you start forward trajectories from a regular grid (no matter how dense), the result (no matter how long the calculations) is an irregular distribution of endpoints.

If you start from a regular grid and go backwards, the endpoints are similarly irregular.

The application called Reverse Domain Fill (RDF) starts backward trajectories from a dense regular grid, and produces a distribution of endpoints.

Take observations that you have and interpolate to this distribution.

Page 13: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Reverse Domain Filling (RDF)

•Step 1Run a back trajectories starting with a regular gridded array

•Step 2 Interpolate observations to back trajectory points

•Step 3Copy values forward to regular grid

•Step 1Run a back trajectories starting with a regular gridded array

•Step 2 Interpolate observations to back trajectory points

•Step 3Copy values forward to regular grid

Time T

Time T-T

Regular grid

Page 14: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

RDF Calculations

Wave breaking features are better resolved

PV is higher

Smoothed RDF not the same as analyzed PV

Wave breaking features are better resolved

PV is higher

Smoothed RDF not the same as analyzed PV

Diabatic

Adiabatic

5o box car smoothed

Page 15: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

N2O 1150 K Jan 11, 1992Gridded ISAMS RDF from Jan 10 RDF from Jan 9

RDF from Jan 5 RDF from Jan 4

RDFs for Jan 11 are calculated using back trajectories from an equal area grid. Back trajectories are 1 to 7 days duration. Each day’s data from the terminus of the back trajectory is projected to the equal area grid. Filamentary structures appear as the back trajectory duration lengthens.

Sutton et al., High Resolution Stratospheric Tracer Fields Estimated from Satellite Observations Using Lagrangian Trajectory Calculations, JAS 1994.

Page 16: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

The left panel RDF for January 7 projects gridded ISAMS data from January 2. The center panel RDF for the same day) projects the along-track data from January 2. The right hand panel is the along-track data (Jan. 2).

The main features are the same in (a) and (b) (disregarding the missing data), showing that the winds play the predominant role in producing the RDF structure, not fine structure from the along-track observations.

Page 17: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

In January/February this year a DC-8 mission took place out of Pease New Hampshire (Polar Aura Validation Experiment PAVE).

One of the instruments on the DC-8 is an ozone lidar AROTEL.The DC-8 flight track nearly coincided with the Aura track for the Microwave Limb Sounder.

The GSFC Chemistry and Transport Model used winds and temperatures from Goddard’s Global Modeling and Assimilation Office meteorological fields to simulate ozone (and other constituents). GMAO assimilated fields are 1 lat x 1.25 long horizontal resolution.

The CTM is usually run at 2 lat x 2.5 long to meet computing constraints.

Page 18: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

MLS (upper left) and AROTAL (lower left) show a sharp vortex edge.

CTM edges are sharper at 1x1.25 (upper right) than at 2x2.5 (lower right), but not nearly as sharp as observed.

1x1.25

2 x 2.5

Page 19: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

A few days later, MLS and AROTAL show a structure (a filament) that is also apparent in the 1x1.25 CTM but only vaguely hinted at in the 2x2.5 CTM.

At 2 x 2.5 the grid point model “overmixes”. Does this matter to O3 evolution (or to a global predictive model?)

1x1.25

2 x 2.5

Page 20: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

2 Days 6 Days

10 Days15 Days

Page 21: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

The RDFs show that the GMAO winds contain the information to produce a filament that looks like the observed filament.

At the same time, the RDFs show more and more structure as the “mixing free” calculation goes back farther and farther in time. This gives a sense of the importance of mixing processes in the stratosphere - there is *too much* structure in the RDF for the longest back trajectories.

How, when, where do parcels mix?

Can models simulate mixing on appropriate temporal and spatial scales?

Page 22: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Lagrangian Mixing Algorithms

• RDF’s can produce infinitely fine structure - such fine structure is not observed => must mix parcels at some point

• Mixing algorithm types– Proximity algorithms

• Parcels which move within a certain distance mix with neighbors

– Conditional Algorithms• Nearby parcels mix under certain flow conditions (most useful

when small number of parcels used)

Page 23: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Proximity Algorithm

Radius of interactionR

Parcels Mix

D=R2/tD = diffusion coefficient

t

Page 24: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

McKenna et al., A new Chemical Lagrangian Model of the Stratosphere (CLaMS) 1. Formulation of

advection and mixing, J. Geophys. Res., 107, 2002.

The CLaMS model was constructed to take advantage of the high spatial resolution afforded by the RDF approach, and at the same time to simulate mixing processes that also play a role in constituent distributions.

The CLaMS mixing scheme has the following properties• ability to represent the scale collapse associated with a 2D turbulent flow• mixing rates depend on the flow pattern and are smallest where the deformation rate is smallest (and vice versa)

Page 25: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

t=t0 t=t0+t

The Lyapunov exponent is the mean logarithmic expansion rate of the principal axes

λ±=±1

Δtln

r0

Start with a uniform grid - think of a grid point as enclosed by a circle

After some time the circle is distorted into an ellipse.

The Lyapunov exponent varies (e.g., small at transport barriers, larger in the surf zone). The CLaMS algorithm “mixes” when the Lyapunov exponent exceeds a critical value.

Page 26: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

N2O 700 K November 10t = 12 hours“low resolution” r0 ≈ 200 km (7000 grid points)

220200180160140120100 80 60 40 20 0

N2O (ppbv)

“pure” advection (no mixing) λc = ∞

Moderate mixing λc = 1.2 days-1

Excessive mixing λc = 0.6 days-1

Page 27: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

CH4 at 475 K on April 8 after 44 days simulation.

CLaMS low resolution simulation (r0 ≈ 200 km)

CLaMS high resolution simulation r0 ≈ 60 km

Isentropic advection using Prather’s numerical transport scheme

1.591.511.431.351.271.191.111.030.95

CH4 (ppmv)

Page 28: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

CLaMS produces structure in this simulation of ozone change for winter 1999/2000 at 450K. Ozone loss is sensitive to chlorine deactivation (ClO + NO2 + M ClONO2 + M) and denitrification, both of which are sensitive to excess mixing.

Page 29: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Winds contain the information to produce filaments

In some cases, maintaining the separation of air masses and structure is important to the photochemical processes.

Importance of this sort of structure to the global scale is less clear and a present topic of investigation.

Page 30: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Massive numbers of trajectories give insight into the overall transport properties of meteorological fields (whether from a data assimilation system or a general circulation model).

Schoeberl et al. used diabatic and kinematic trajectories to compare tropical transport produced by UKMO and GEOS data assimilation systems.

Diabatic trajectories • parcels transported along isentropic surfaces by the large-scale wind field• parcels moved across isentropic surfaces by the net diabatic heating

Kinematic trajectories• parcels transorted horizontally on pressure surfaces• parcels moved vertically by the omega field (dp/dt, where p is the pressure)

Schoeberl et al., A comparison of the lower stratospheric age spectra derived from a general circulation model and two data assimilation system, J. Geophys. Res., 108, 2003

Page 31: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center
Page 32: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center
Page 33: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

These trajectory calculations clearly show the problems with the meteorological data sets.

Both diabatic and kinematic trajectories for UKMO and FVDAS show that the air in the central tropics comes from middle latitude - this level of horizontal mixing is not support by aircraft or satellite observations.

It is important that using the heating rates to specify the vertical transport does not solve the problem. Although either of these simulations will behave more physically at polar latitudes when the vertical transport is specified by the heating rates, there are issues with mixing and mass balance that affect the simulations and affect comparisons of simulated and observed constituent fields.

Page 34: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center

Summary

The trajectory approach is an important tool in process study land. Trajectories

– can provide insight into photochemical processes through application to interpretation of measurements

– can provide insight into transport and mixing processes– can reveal large scale characteristics of atmospheric flow

The trajectory approach has some issues/limitations: – position errors– mixing issues– tropospheric processes (convection, clouds, boundary layer)

The trajectory approach will serve the user best if s/he understands the limitations and avoids the pitfalls of the “black box”.

Page 35: Lagrangian Models Anne Douglass Code 613.3 Atmospheric Chemistry and Dynamics Branch NASA Goddard Space Flight Center