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 |
You must register with us as either a Registered User before you can Download this Book. You'll be greeted by a simple sign-up page.
Once you have finished the sign-up process, you will be redirected to your download Book page.
How it works: