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Assessment of Fast-Time Wake Vortex Prediction ModelsFast-time wake prediction models are semi-empirical, and are designed to predict aircraft wake vortex information behind a generating aircraft. They are developed using theoretical concepts and often calibrated with data obtained from field measurements, laboratory studies, or numerical simulations. They rely upon inputs representing the generating aircraft (such as weight, airspeed, wingspan, lateral position, and altitude) and atmospheric environment (such as ambient winds, turbulence, and temperature lapse rate). Other input may include the type of aircraft (e.g., B-747- 400). Output from these models may include time histories of the wake vortex strength, and position, as well as a prediction of the uncertainties in strength and position. Fast-time models should provide solutions in a fraction of a second, and hence is an enabling technology able to perform in a real-time operational system, such as dynamic spacing systems envisioned by the Aircraft Vortex Spacing System or other Super Density Operations concepts. Other applications of fast-time models include 1) guidance for wake separation standards for new aircraft, 2) optimization of separation standards for existing aircraft, 3) guidance for setting vertical separation standards during cruise, 4) accident reconstructions, and 5) testing of new concepts for safe increases in airport capacity for both single and multiple runway configurations. Fast-time models are based on a number of assumptions which limit their accuracy and range of application. For example, they do not predict the meandering vortex paths that can result from the wake interaction with atmospheric turbulence. However, these models should account for the mean vortex position and may predict the level of uncertainty.

This presentation describes a study in which comparative evaluations of fast-time wake transport and decay models were conducted using data sets from previous field programs taken at MEM (1995), DFW (1997, 1999, 2000), and Denver (2005, 2006) airports. These data sets contain, meteorological data, lidar measurements of wake vortices, and the aircraft parameters associated with these vortices.
Document ID
20200004911
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Fred H Proctor
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 11, 2020
Publication Date
March 29, 2011
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
Report Number: NF1676L-12387
NF1676L-12387
Meeting Information
Meeting: NASA Airspace Systems Program Technical Interchange Meeting
Location: San Diego, CA
Country: US
Start Date: March 29, 2011
End Date: March 31, 2011
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 411931.02.61.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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