Static investigation of a multiaxis thru
Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability
David J. Wing
March to the Grave
Afterbody/nozzle pressure distributions
Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2
Internal performance of a nonaxisymmetri
Internal performance of a nonaxisymmetric nozzle with a rotating upper flap and a center-pivoted lower flap
Performance characteristics of two multi
Performance characteristics of two multiaxis thrust-vectoring nozzles at Mach numbers up to 1.28
Static investigation of two fluidic thru
Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle
Static performance investigation of a sk
Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept
Static performance of a cruciform nozzle
Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities
Static thrust and vectoring performance
Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct
Autonomous flight rules
Fantasia Divinity Magazine: Issue 13, August 2017: Anniversary Edition
