Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnelRichard J. Re · First published 1998Open the Tome
A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92Richard J. Re · First published 1996Open the Tome
Wind tunnel investigation of three axisymmetric cowls of different lengths at Mach numbers from 0.60 to 0.92Richard J. Re · First published 1993Open the Tome
Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraftRichard J. Re · First published 1991Open the Tome
Effect of varying internal geometry on the static performance of rectangular thrust-reverser portsRichard J. Re · First published 1987Open the Tome
Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flapRichard J. Re · First published 1986Open the Tome
Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzlesRichard J Re · First published 1984Open the Tome
Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parametersRichard J Re · First published 1984Open the Tome
Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversingRichard J Re · First published 1982Open the Tome
Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configurationRichard J. Re · First published 1979Open the Tome
Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20Richard J. Re · First published 1978Open the Tome
An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90Richard J Re · First published 1977Open the Tome
