Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilitiesLaurence D. Leavitt · First published 1985Open the Tome
Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60⁰Laurence D. Leavitt · First published 1985Open the Tome
Effect on empennage location on twin-engine afterbody/nozzle aerodynamic characteristics at Mach numbers from 0.6 to 1.2Laurence D. Leavitt · First published 1983Open the Tome
Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristicsLaurence D. Leavitt · First published 1983Open the Tome
Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flapsLaurence D. Leavitt · First published 1982Open the Tome
Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzlesLaurence D. Leavitt · First published 1982Open the Tome
Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speedsLaurence D. Leavitt · First published 1979Open the Tome
Effects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speedsLaurence D. Leavitt · First published 1978Open the Tome
