NASA NTRS · 20000044622
HSR High-Lift Technology Overview
Abstract
High-lift system performance will have a large impact on airplane noise and weight. Successful completion of PCD1 activities provided greater understanding of aerodynamic characteristics and configuration features important to high-lift system performance including: 1) Reynolds number effects (Ref. H); 2) Propulsion/airframe integration effects; and 3) Planform effects, canard/3-surface, alternate high-lift concepts, etc. PCD2 plans are aimed at achieving technology development performance goals and increasing technology readiness level for Technology Concept.
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Applin, Z. T.. 1999-12-01. HSR High-Lift Technology Overview. https://ntrs.nasa.gov/citations/20000044622
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