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Three-dimensional wings of minimum pressure dragIn linearized flow theory, certain very interesting extremal properties of wings can be derived under rather broad conditions without the use of a complicated mathematical apparatus. The present chapter reviews certain results of this theory and indicates some rather obvious extensions to incorporate various auxiliary conditions. Several examples illustrating the relation between the geometrical features of the wing and the lift distribution for minimum drag are given.
Document ID
19760012014
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jones, R. T.
(Avco-Everett Research Lab. MA, United States)
Date Acquired
August 8, 2013
Publication Date
February 1, 1976
Publication Information
Publication: NASA. Ames Res. Center Collected Works of Robert T. Jones
Subject Category
Aerodynamics
Accession Number
76N19102
Distribution Limits
Public
Copyright
Public Use Permitted.
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