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Cost consideration for aircraft configuration changes, 1The costs of improvements in aircraft drag reduction design changes are outlined in the context of production decisions. A drag reduction design with increased airframe weight requires cost increases for direct labor, overhead and direct expenses, plus general and administrative expenses.
Document ID
19760003934
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tumlinson, R. R.
(Beech Aircraft Corp. Wichita, KS, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Kansas Univ. Proc. of the NASA, Ind., Univ., Gen. Aviation Drag Reduction Workshop
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N11022
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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