David J. Wing

Afterbody/nozzle pressure distrib...

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

Year unknown

Autonomous flight rules

Autonomous flight rules

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

Year unknown Amber M. Simpson, Nidhi Singh, DC Diamondopolous, Kristyl Gravina, David J. Wing, Karen Heslop, Brett Petersen, Elana Gomel, J.M. Williams, EJ Shumak, and Mike Murphy

Internal performance of a nonaxis...

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

Year unknown

March to the Grave

Year unknown Christopher Pulo, Pete Clark, David J. Wing, Gary L. Robbe, Gerry Huntman, Phoebe Reeves-Murray, and Deborah Sheldon

Performance characteristics of tw...

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

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Static investigation of a multiax...

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

Year unknown

Static investigation of two fluid...

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

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Static performance investigation ...

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

Year unknown

Static performance of a cruciform...

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

Year unknown

Static thrust and vectoring perfo...

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

Year unknown