A System for Aerodynamic Design and Analysis of Supersonic Aircraft: User's manual

A System for Aerodynamic Design and Analysis of Supersonic Aircraft: User's manual

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In addition, it has been found that, for a wing alone case, the wing root singularity and the corresponding root camber line can often be moderated by substituting a parabolic apex for the sharp apex common to supersonic wing planforms. This will be performed automatically in the program if the input YSN00T is not zero. The program then fits a parabola tangent to the wing leading edge at YSN00T, with symmetry about Y=0. Because the computed camber surface slopes tend to exhibitanbsp;...


Title:A System for Aerodynamic Design and Analysis of Supersonic Aircraft: User's manual
Author: Wilbur D. Middleton, J. L. Lundry, Ronald Gene Coleman, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Publisher: - 1980
ISBN-13:

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