Study of shaping of bodies for different Mach numbers; wing, designed to have high performance characteristics when used with indented body, was tested in combination with unindented body and bodies for 1.0, 1.2, and 1.4 Mach; lowest values of zero lift wave drag and highest values of maximum lift drag ratio were obtained at or near Mach number for given indentations.
Transonic investigation of changing indentation design Mach number on aerodynamic characteristics of 45° sweptback-wing-body combination designed for high performance
NASA -- Tech Note
1961
86 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.