Research conducted during the period from July 1991 through December 1992 is covered. A method based upon the quasi-analytical approach was developed for computing the aerodynamic sensitivity coefficients of three dimensional wings in transonic and subsonic flow. In addition, the method computes for comparison purposes the aerodynamic sensitivity coefficients using the finite difference approach. The accuracy and validity of the methods are currently under investigation.
An initial investigation into methods of computing transonic aerodynamic sensitivity coefficients
01.02.1992
Report
Keine Angabe
Englisch
Transonic Blunt Body Aerodynamic Coefficients Computation
British Library Conference Proceedings | 2011
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