Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent ductDavid J. Wing · First published 1998Open the Tome
Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring abilityDavid J. Wing · First published 1997Open the Tome
Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2David J. Wing · First published 1995Open the Tome
Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzleDavid J. Wing · First published 1994Open the Tome
Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle conceptDavid J. Wing · First published 1994Open the Tome
Internal performance of a nonaxisymmetric nozzle with a rotating upper flap and a center-pivoted lower flapDavid J. Wing · First published 1993Open the Tome
Performance characteristics of two multiaxis thrust-vectoring nozzles at Mach numbers up to 1.28David J. Wing · First published 1993Open the Tome
Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilitiesDavid J. Wing · First published 1992Open the Tome
