Analysis and numerical computaton of sensitivity derivatives in the transonic regime /

The incremental iterative technique is implemented to solve the sensitivity equations, and, thus, improve the concept that it is possible to efficiently couple for three dimensional transonic flow about an unswept and twisted rectangular wing an aerodynamic solution for the pressure distribution wit...

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Bibliographic Details

Main Author:	Arslan, Alain Elie, 1969-
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 1993.
Subjects:	Major aerospace engineering.
Online Access:	Link to OAKTrust copy