NASA NTRS · 19800000092
Disturbance amplification rates
Abstract
Program computes incompressible linear stability characteristics for swept and tapered wings. Amplification rates of boundary-layer disturbances also are calculated. Program is useful in designing tapered, laminar-flow control wings incorporating suction to prevent boundary layer separation. Program is written in FORTRAN IV and Assembler for batch execution on CYBER 70-series.
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Srokowski, A. J., Orszag, S. A., Cebech, T., Kaups, K.. 1980-08-01. Disturbance amplification rates. https://ntrs.nasa.gov/citations/19800000092
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