NASA NTRS · 19780019125
Development of advanced stability theory suction prediction techniques for laminar flow control
Abstract
The problem of obtaining accurate estimates of suction requirements on swept laminar flow control wings was discussed. A fast accurate computer code developed to predict suction requirements by integrating disturbance amplification rates was described. Assumptions and approximations used in the present computer code are examined in light of flow conditions on the swept wing which may limit their validity.
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Srokowski, A. J.. 1978-06-01. Development of advanced stability theory suction prediction techniques for laminar flow control. https://ntrs.nasa.gov/citations/19780019125
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