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Computer program for steamtube curvature analysis: Analytical methodProgram provides design information for low-drag, high-drag-divergence, Mach number isolated nacelles suitable for use with advanced high-bypass-ratio, turbofan engines. One element is development of method to predict inviscid pressure distribution and flow field about arbitrary axisymmetric ducted body at transonic speeds.
Document ID
19740000206
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Ferguson, D. R. (GE)
Heck, P. H. (GE)
Keith, J. S. (GE)
Lahti, D. J. (GE)
Merkle, C. L. (GE)
Date Acquired
August 7, 2013
Publication Date
November 1, 1974
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LAR-11535
Report Number: LAR-11535
Accession Number
74B10206
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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