NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Analysis of aircraft performance during lateral maneuvering for microburst avoidanceAircraft response to a severe and a moderate three-dimensional microburst model using nonlinear numerical simulations of a Boeing 737-100 is studied. The relative performance loss is compared for microburst escape procedures with and without lateral maneuvering. The results show that the hazards caused by the penetration of a microburst in the landing phase are attenuated if lateral escape maneuvers are applied in order to turn the aircraft away from the microburst core rather than flying straight through. If the lateral escape maneuver is initiated close to the microburst core, high bank angles tend to deteriorate aircraft performance. Lateral maneuvering is also found to reduce the advanced warning required to escape from microburst hazards but requires that information of the existence and location of the microburst is available (i.e., remote detection) in order to avoid an incorrect turn toward the microburst core.
Document ID
19900032865
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Avila De Melo, Denise
(Embraer S.A., Sao Jose dos Campos, Brazil)
Hansman, R. John, Jr.
(MIT Cambridge, MA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 90-0568
Accession Number
90A19920
Funding Number(s)
CONTRACT_GRANT: NAG1-690
CONTRACT_GRANT: NGL-22-009-640
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available