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Technical Paper (8) Journal Article (4)

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Aerospace (8)

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Aerodynamics (6) Unmanned aerial vehicles (6) Wings (6) Munitions (4) Aircraft (3) Education and training (3) Research and development (3) CAD, CAM and CAE (2) Knock (2) Pitch (2) Roll (2) Wind tunnel tests (2) Assembling (1) Computational fluid dynamics (CFD) (1) Computer software and hardware (1) Control systems (1) Drag (1) Durability (1) Flight tests (1) Fuselages (1) Identification (1) Imaging and visualization (1) Mathematical models (1) Propellants (1) Sensors and actuators (1) Simulators (1) Vehicle acceleration (1) Yaw (1)

Authors

Huebsch, Wade (12) Wilhelm, Jay (7) Gautam, Mridul (5) Browning, Patrick H. (4) Browning, Patrick (3) Hamburg, Shanti (2) Cain, Richard (1) Cain, Richard Brian (1) Close, Joesph (1) Close, Joseph (1) Dennison, Hunter James (1) Gioia, Christopher (1) Griffin, Christopher (1) Guiler, Richard (1) Jakkali, Vinay (1) LaBarbara, Kirk (1) Minehart, Robert F. (1) Robert, Ashish (1)

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SAE (12)

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West Virginia University (8) West Virginia Univ. (3) WVU Research Corporation (1) West Virginia University, Department of Mechanical and Aerospace Engineering (1)

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SAE 2013 AeroTech Congress & Exhibition (5) Aerospace Technology Conference and Exposition (4) AeroTech Conference & Exhibition (1) SAE 2014 Aerospace Systems and Technology Conference (1) SAE 2015 AeroTech Congress & Exhibition (1)

Search Results (12) Search History

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Select Design, Construction, and Operation of a Pneumatic Test Launch Apparatus for sUAS Prototypes

Design, Construction, and Operation of a Pneumatic Test Launch Apparatus for sUAS Prototypes

Technical Paper
2015-01-2454
DOI: https://doi.org/10.4271/2015-01-2454

Published 2015-09-15 by SAE International in United States

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Select Investigation of Dynamic Roughness Flow Control on NACA 0012 Airfoil at Low Reynolds Number

Investigation of Dynamic Roughness Flow Control on NACA 0012 Airfoil at Low Reynolds Number

Technical Paper
2013-01-2096
DOI: https://doi.org/10.4271/2013-01-2096

Published 2013-09-17 by SAE International in United States

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Select Investigation of Faceted Wing Sections for Low Reynolds Number Applications

Investigation of Faceted Wing Sections for Low Reynolds Number Applications

Technical Paper
2013-01-2097
DOI: https://doi.org/10.4271/2013-01-2097

Published 2013-09-17 by SAE International in United States

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Select Hybrid Projectile Transformation Condition Detection System for Extended Selectable Range

Hybrid Projectile Transformation Condition Detection System for Extended Selectable Range

Technical Paper
2013-01-2203
DOI: https://doi.org/10.4271/2013-01-2203

Published 2013-09-17 by SAE International in United States

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Select Guidance and Range Extension Control System for a Hybrid Projectile

Guidance and Range Extension Control System for a Hybrid Projectile

Technical Paper
2014-01-2175
DOI: https://doi.org/10.4271/2014-01-2175

Published 2014-09-16 by SAE International in United States

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Select A Comparison of Wing Stowing Designs Focused on Increased Continuous Payload Volume for Projectile Applications

A Comparison of Wing Stowing Designs Focused on Increased Continuous Payload Volume for Projectile Applications

Technical Paper
2011-01-2782
DOI: https://doi.org/10.4271/2011-01-2782

Published 2011-10-18 by SAE International in United States

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Select Development and Testing of a Wing Morphing Mechanism for the Control of a Swept Wing Tailless Aircraft

Development and Testing of a Wing Morphing Mechanism for the Control of a Swept Wing Tailless Aircraft

Technical Paper
2005-01-3391
DOI: https://doi.org/10.4271/2005-01-3391

Published 2005-10-03 by SAE International in United States

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Select Investigation of Small Scale Pulsed Detonation Engines and Feasibility Study for Implementation with Disposable Unmanned Aerial Systems

Investigation of Small Scale Pulsed Detonation Engines and Feasibility Study for Implementation with Disposable Unmanned Aerial Systems

SAE International Journal of Aerospace

Journal Article
2013-01-2304

Published 2013-09-17 by SAE International in United States

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Select A De-Spin and Wings-Leveling Controller for a 40 mm Hybrid Projectile

A De-Spin and Wings-Leveling Controller for a 40 mm Hybrid Projectile

SAE International Journal of Aerospace

Journal Article
2013-01-2262

Published 2013-09-17 by SAE International in United States

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Select An Experimental Investigation of the Transient Effects Associated with Wing Deployment During Ballistic Flight

An Experimental Investigation of the Transient Effects Associated with Wing Deployment During Ballistic Flight

SAE International Journal of Aerospace

Journal Article
2011-01-2647

Published 2011-10-18 by SAE International in United States

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