Book Description

The TranAir computer program calculates transonic flow about arbitrary configurations at subsonic, transonic, and supersonic freestream Mach numbers. TranAir solves the nonlinear full potential equations subject to a variety of boundary conditions modeling wakes, inlets, exhausts, porous walls, and impermeable surfaces. Regions with different total temperature and pressure can be represented. The user's manual describes how to run the TranAir program and its graphical support programs. Johnson, F. T. and Samant, S. S. and Bieterman, M. B. and Melvin, R. G. and Young, D. P. and Bussoletti, J. E. and Hilmes, C. L. Unspecified Center NASA-CR-4349, A-90092, NAS 1.26:4349 NAS2-12513; RTOP 505-61-21...