Development of High-rate, Adaptive Trailing Edge Control Surface for the Smart Wing Phase 2 Wind Tunnel Model

Development, control, and test results of high-rate hingeless trailing edge-control surface for the Smart Wing Phase 2 wind tunnel model

10.1117/12.475100 ◽

2002 ◽

Cited By ~ 8

Author(s):

Jonathan D. Bartley-Cho ◽

Donny P. Wang ◽

Mark N. West

Keyword(s):

Wind Tunnel ◽

High Rate ◽

Control Surface ◽

Phase 2 ◽

Test Results ◽

Trailing Edge ◽

Wind Tunnel Model ◽

Development Control ◽

Development of high-rate large-deflection hingeless trailing-edge control surface for the Smart Wing wind tunnel model

10.1117/12.429682 ◽

2001 ◽

Cited By ~ 12

Author(s):

Donny P. Wang ◽

Jonathan D. Bartley-Cho ◽

Christopher A. Martin ◽

Brian J. Hallam

Keyword(s):

Wind Tunnel ◽

Large Deflection ◽

High Rate ◽

Control Surface ◽

Trailing Edge ◽

Wind Tunnel Model ◽

Multi-Material Printed Trailing Edge Control Surface for an Aeroservoelastic Wind Tunnel Model

2018 Multidisciplinary Analysis and Optimization Conference ◽

10.2514/6.2018-2930 ◽

2018 ◽

Cited By ~ 4

Author(s):

Alexander M. Pankonien ◽

Ryan Durscher ◽

Nitin D. Bhagat ◽

Gregory Reich

Keyword(s):

Wind Tunnel ◽

Control Surface ◽

Trailing Edge ◽

Wind Tunnel Model ◽

The design, construction, and tests of a concept aeroelastic wind tunnel model of a high-lift variable camber continuous trailing edge flap (HL-VCCTEF) wing configuration

56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ◽

10.2514/6.2015-1406 ◽

2015 ◽

Cited By ~ 14

Author(s):

Nathan Precup ◽

Marat Mor ◽

Eli Livne

Keyword(s):

Wind Tunnel ◽

Trailing Edge ◽

High Lift ◽

Wind Tunnel Model ◽

Tunnel Model ◽

Trailing Edge Flap ◽

Design Construction

Design, fabrication, and testing of scaled wind tunnel model for the Smart Wing Phase 2 program

10.1117/12.475091 ◽

2002 ◽

Cited By ~ 3

Author(s):

Christopher A. Martin ◽

Brian J. Hallam ◽

John S. Flanagan ◽

Jonathan D. Bartley-Cho

Keyword(s):

Wind Tunnel ◽

Phase 2 ◽

Wind Tunnel Model ◽

Control Surface Response of a Blended Wing Body Aeroelastic Wind-Tunnel Model

Journal of Aircraft ◽

10.2514/1.5440 ◽

2005 ◽

Vol 42 (3) ◽

pp. 738-742 ◽

Author(s):

Martin Carlsson

Keyword(s):

Wind Tunnel ◽

Control Surface ◽

Wind Tunnel Model ◽

Surface Response ◽

Tunnel Model ◽

Blended Wing Body

An Active Variable Camber Continuous Trailing Edge Flapped Wing Wind Tunnel Model for Aeroelastic "In-Flight" Shape Optimization Tests

2018 Multidisciplinary Analysis and Optimization Conference ◽

10.2514/6.2018-3106 ◽

2018 ◽

Author(s):

Nathan Precup ◽

Marat Mor ◽

Eli Livne

Keyword(s):

Wind Tunnel ◽

Shape Optimization ◽

Trailing Edge ◽

Wind Tunnel Model ◽

Design, Construction, and Tests of an Aeroelastic Wind Tunnel Model of a Variable Camber Continuous Trailing Edge Flap (VCCTEF) Concept Wing

32nd AIAA Applied Aerodynamics Conference ◽

10.2514/6.2014-2442 ◽

2014 ◽

Author(s):

Eli Livne ◽

Nathan Precup ◽

Marat Mor

Keyword(s):

Wind Tunnel ◽

Trailing Edge ◽

Wind Tunnel Model ◽

Tunnel Model ◽

Trailing Edge Flap ◽

Design Construction

47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th ◽

Control surface interaction effects of the Active Aeroelastic Wing wind tunnel model

10.2514/6.2006-2185 ◽

2006 ◽

Author(s):

Jennifer Heeg

Keyword(s):

Wind Tunnel ◽

Interaction Effects ◽

Surface Interaction ◽

Control Surface ◽

Wind Tunnel Model ◽

Aeroelastic Trade Study of a Conformal Control Surface for a Printable Wind Tunnel Model

AIAA Scitech 2019 Forum ◽

10.2514/6.2019-2358 ◽

2019 ◽

Author(s):

Alexander M. Pankonien ◽

Ryan J. Durscher ◽

Nitin Bhagat

Keyword(s):

Wind Tunnel ◽

Control Surface ◽

Wind Tunnel Model ◽

Tunnel Model ◽

Trade Study