Tropical Cyclone Winds at Landfall Experimental Options

This document is divided into FIVE sections:

Real-time Module

The real-time module combines passes over marine surface platforms with one or more figure four patterns in the core of the hurricane. The aircraft flies at or below 5,000 ft (1.5 km) (ideally at 2,500 ft [750 m]), so that flight level winds can be adjusted to 30 ft (10 m) to combine with measurements from marine surface platforms. Flight-level data and GPS-sondes dropped near the platforms will be used to validate the adjustment method. Doppler data collected in the figure four will be analyzed with EVTD in real-time on the HRD workstation. The lowest level of the EVTD analysis may be sent to TPC/NHC where the Doppler winds can also be adjusted to the surface and made available to HRD's real-time surface wind analysis system. Note that if the storm is outside of WSR-88D Doppler range then the figure four pattern could be repeated before returning home.

For example, if a hurricane moves within range of Melbourne, Florida, then the flight pattern should take advantage of buoys 41009 and 41010. The aircraft descends at the initial point and begins a low-level figure-4 pattern, modifying the legs to fly over the buoys (Fig. 20).

Whenever the drift angle permits the radar will be in F/AST mode, except in the eye penetrations. If time permits the aircraft would make one more pass through the eye and then fly the dual-Doppler module. In this example the pattern would be completed in about 2.5 h. GPS-sondes would be dropped near the buoys.

[Return to table of contents above]


Dual-Doppler Option 1

If the TC moves within Doppler range of a coastal WSR-88D 125 nmi (230 km), then we will fly a second module, to collect a time-series of dual-Doppler data from the storm's inner core. Note that the optimal volume scans for this pattern will be obtained when the storm is 32-80 nmi (60-150 km) from the radar, because beyond 80 nmi (150 km) the lowest WSR-88D scan will be above 5,000 ft (1.5 km) which is too high to resolve the low-level wind field. Within 32 nmi (60 km) the volume scan will be incomplete, because the WSR-88D does not scan above 19.5?.

The pattern will depend on the location of the storm relative to the coastal radar. Depending on safety and operational considerations, the aircraft could fly this portion of the experiment at a higher altitude, although 5,000 ft (1.5 km) would still be preferred. Continuing our example for the Melbourne WSR-88D, after completing the real-time module the aircraft flies to an initial point on the track intersecting the storm center and the coastal radar (Fig. 20). The aircraft then makes several passes through the eyewall (A-B in Fig. 20), with the tail radar scanning perpendicularly to the track. Depending on the size of the eyewall each pass should last 10-20 min. It is essential that these passes be flown as straight as possible, because turns to fix the eye will degrade the Doppler radar coverage. After each pass the aircraft turns quickly and heads back along the same track, adjusted to keep the storm center and the coastal radar on the same line. In 2 h, 6-12 volume scans will be collected. The last pass should be followed by a pass through the eye perpendicular to the other legs, to provide data for EVTD and pseudo-dual Doppler analyses. If time permits, the real-time module could be repeated before returning home, or the coastal-survey module could be flown.

[Return to table of contents above]


Dual-Doppler Option 2

If dual-Doppler data are desired over a larger area, then another module will be flown where the aircraft flies along three WSR-88D radials to survey both the inner core and surrounding rainbands (Fig. 21).

In the example shown, this pattern could be flown in about 2 h. Note that the legs outside the inner core should be flown with the tail radar in F/AST mode because the drift angle would be smaller. In the example the module concludes with a coastal-survey pass south along the coast.

[Return to table of contents above]


Coastal Survey Option

When the hurricane is making landfall, this module will provide information about the boundary layer in the onshore and offshore flow regimes. The WP-3D would fly a coastal survey pattern parallel to the coast, as close as safety permits, at 5,000 ft (1.5 km) or less, and drop GPS-sondes on either side of the storm track, to sample both onshore and offshore flow regimes (Fig. 22). The Doppler radar would be in F/AST mode, to provide wind estimates on either side of the aircraft track. This module could be flown when the hurricane is making landfall or after the storm moves inland. The pattern could be flown in ~1 h. GPS-sonde drops could be adjusted to be near surface platforms.

[Return to table of contents above]


Post-landfall Option

If the structure of the storm is such that flight patterns at 10,000 or 15,000 ft (3.0 or 4.5 km) are feasible over land, the pattern shown in Dual Doppler option 1 would be flown, except that the storm would be followed inland as long as time and safety considerations permit. It may be possible to fly the radial legs with the radar in F/AST scanning mode depending on the location and status of the WSR-88D.

[Return to table of contents above]


Back to the Tropical Cyclone Winds at Landfall Experiment