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The role of simulation in determining safe aircraft landing separation criteriaThe role of flight simulation in determining safe aircraft landing separation criteria is reviewed and discussed. A broad conclusion is made that previous vortex-encounter simulations were useful for predicting the general response of an aircraft in the presence of trailing vortices and the type of separation criteria to emphasize. These simulations, however, were generally limited in scope and validation. Broad requirements for an accepted simulation methodology are presented. Key technological issues are addressed, including the addition of high-fidelity vortex models and aircraft/vortex interaction effects in the simulation, and validation of simulations with experimental data. Finally, results from a preliminary one-degree-of-freedom simulation are shown. These indicate that reduced landing spacings may be feasible and that current aircraft categorizations should be reviewed.
Document ID
19930034715
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stuever, Robert A.
(NASA Langley Research Center Hampton, VA, United States)
Stewart, Eric C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
October 1, 1991
Subject Category
Air Transportation And Safety
Meeting Information
Meeting: FAA, International Wake Vortex Symposium
Location: Washington, DC
Country: United States
Start Date: October 29, 1991
End Date: October 31, 1991
Sponsors: FAA
Accession Number
93A18712
Distribution Limits
Public
Copyright
Other

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