David J. Wing

Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability

March to the Grave

Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2

Autonomous flight rules

Fantasia Divinity Magazine: Issue 13, August 2017: Anniversary Edition

Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities

Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle

Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct

Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept

Internal performance of a nonaxisymmetric nozzle with a rotating upper flap and a center-pivoted lower flap

Performance characteristics of two multiaxis thrust-vectoring nozzles at Mach numbers up to 1.28