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Runway Exit Designs for Capacity Improvement Demonstrations. Phase 1: Algorithm DevelopmentA description and results are presented of a study to locate and design rapid runway exits under realistic airport conditions. The study developed a PC-based computer simulation-optimization program called REDIM (runway exit design interactive model) to help future airport designers and planners to locate optimal exits under various airport conditions. The model addresses three sets of problems typically arising during runway exit design evaluations. These are the evaluations of existing runway configurations, addition of new rapid runway turnoffs, and the design of new runway facilities. The model is highly interactive and allows a quick estimation of the expected value of runway occupancy time. Aircraft populations and airport environmental conditions are among the multiple inputs to the model to execute a viable runway location and geometric design solution. The results presented suggest that possible reductions on runway occupancy time (ROT) can be achieved with the use of optimally tailored rapid runway designs for a given aircraft population. Reductions of up to 9 to 6 seconds are possible with the implementation of 30 m/sec variable geometry exits.
Document ID
19910007752
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Trani, A. A.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Hobeika, A. G.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Sherali, H.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Kim, B. J.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Sadam, C. K.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1990
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-187955
CTR-R-1-90-PHASE-1
AD-A231498
NAS 1.26:187955
DOT/FAA/RD-90/32-PHASE-1
Report Number: NASA-CR-187955
Report Number: CTR-R-1-90-PHASE-1
Report Number: AD-A231498
Report Number: NAS 1.26:187955
Report Number: DOT/FAA/RD-90/32-PHASE-1
Accession Number
91N17065
Funding Number(s)
CONTRACT_GRANT: NAS1-18471
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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