Aeropulsive Characteristics at Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model

Download or read book Aeropulsive Characteristics at Mach Numbers Up to 2.2 of Axisymmetric and Nonaxisymmetric Nozzles Installed on an F-18 Model written by Francis J. Capone and published by . This book was released on 1982 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation to determine the aeropropulsive characteristics of nonaxisymmetric nozzles on an F-18 jet effects model was conducted in the Langley 16-foot transonic tunnel and the AEDC 16-foot supersonic wind tunnel. The performance of a two dimensional convergent-divergent nozzle, a single expansion ramp nozzle, and a wedge nozzle was compared with that of the baseline axisymmetric nozzle. Test data were obtained at static conditions and at Mach numbers from 0.60 to 2.20 at an angle of attack of 0 deg. Nozzle pressure ratio was varied from jet-off to about 20.