David J. Wing

· 11 obras en el catálogo

Obras

AAfterbody/nozzle pressure distributions of a twin-tail twin-

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

IInternal performance of a nonaxisymmetric nozzle with a rota

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

PPerformance characteristics of two multiaxis thrust-vectorin

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

SStatic investigation of two fluidic thrust-vectoring concept

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

SStatic performance investigation of a skewed-throat multiaxi

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

SStatic performance of a cruciform nozzle with multiaxis thru

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

SStatic thrust and vectoring performance of a spherical conve

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

SStatic investigation of a multiaxis thrust-vectoring nozzle

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

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

March to the Grave

AAutonomous flight rules

Autonomous flight rules