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Disturbance amplification ratesProgram 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.
Document ID
19800000092
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Srokowski, A. J. (Cambridge Hydrodynamics, Inc.)
Orszag, S. A. (McDonnell Douglas)
Cebech, T. (McDonnell Douglas Corp.)
Kaups, K.
Date Acquired
August 10, 2013
Publication Date
August 1, 1980
Publication Information
Publication: NASA Tech Briefs
Volume: 5
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12556
ISSN: 0145-319X
Report Number: LAR-12556
Accession Number
80B10092
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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