To determine effect of acceleration on development of lift in simulated carrier-deck catapult takeoff for 2-dimensional wing, unswept wing, swept and delta planform wing; each of wings developed 90% of its steady-state lift within 7 chord lengths of travel; results agreed qualitatively with those calculated from theory.
Wind-tunnel investigation of development of lift on wings in accelerated longitudinal motion
NASA -- Tech Note
1960
16 pages
Report
Englisch
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