Wilbur D. Middleton, J. L. Lundry, Ronald Gene Coleman, United States. ... solves for drag-due-to-lift, lift-curve slope, and pitching moment characteristics of a given configuration through a range of angles of attack at a selected Mach number.
|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|