Optimization of a Seamless Inlet Liner Using an Empirically Validated Prediction Method
Author:
Affiliation:
1. Honeywell International, Inc.
2. GKN Aerospace
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3824
Reference11 articles.
1. An Integrated Optimization System for Low Noise Nacelle Design
2. 4FreeFieldTechnologies,ACTRAN10User'sManual,FFT,Brussels,Belgium,2010.
3. 5Weir,D."EngineValidationofNoiseandEmissionReductionTechnologyPhaseI,"NASACR2008-215225.
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