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Prospects and time tables for analytical estimation of the drag of complete aircraft configurationAnalytical drag methods and wind tunnel evaluation of aircraft design features are used to identify excessive drag of general aviation aircraft with reciprocating engines.
Document ID
19760003911
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smetana, F. O. (North Carolina State Univ. Raleigh, NC, 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
Aerodynamics
Accession Number
76N10999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19760003909Collected WorksProceedings of the NASA, Industry, University, General Aviation Drag Reduction Workshop
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