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.
Disturbance amplification rates
NASA Tech Briefs ; 5 , 1
1980-08-01
Miscellaneous
No indication
English
Amplification at a disturbance wave-head in a homogeneous explosion
Elsevier | 1977
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