Wing configuration

Results: 63



#Item
41Flight Line The Official Publication of the CAF Southern California Wing 455 Aviation Drive, Camarillo, CA[removed]0064 Vol. XXXI No. 1

Flight Line The Official Publication of the CAF Southern California Wing 455 Aviation Drive, Camarillo, CA[removed]0064 Vol. XXXI No. 1

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Source URL: www.orgsites.com

Language: English - Date: 2011-01-09 23:37:18
42Robert H. Liebeck Bob Liebeck is currently manager of the Blended-Wing-Body (BWB) Airplane Program at Boeing. The BWB is an advanced concept subsonic transport configuration that offers

Robert H. Liebeck Bob Liebeck is currently manager of the Blended-Wing-Body (BWB) Airplane Program at Boeing. The BWB is an advanced concept subsonic transport configuration that offers

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Source URL: 158.132.173.15

Language: English - Date: 2011-04-20 23:14:09
43DEPARTMENT OF AUTOMOTIVE AND AERONAUTICAL ENGINEERING  Conceptual Design of a Medium Range Box Wing

DEPARTMENT OF AUTOMOTIVE AND AERONAUTICAL ENGINEERING Conceptual Design of a Medium Range Box Wing

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Source URL: www.fzt.haw-hamburg.de

Language: English - Date: 2011-01-06 12:57:25
44DRDO Science Spectrum, March 2009, pp[removed]DRDO SCIENCE SPECTRUM 2009 © 2009, DESIDOC

DRDO Science Spectrum, March 2009, pp[removed]DRDO SCIENCE SPECTRUM 2009 © 2009, DESIDOC

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Source URL: drdo.gov.in

Language: English - Date: 2011-04-29 07:18:19
45IS  TO

IS TO

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Source URL: www.nasa.gov

Language: English - Date: 2013-08-15 12:25:37
46Flight Safety D

Flight Safety D

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Source URL: www.skybrary.aero

Language: English - Date: 2008-07-20 04:34:56
47NASA/CR[removed]Modeling and Optimization for Morphing

NASA/CR[removed]Modeling and Optimization for Morphing

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Source URL: ntrs.nasa.gov

Language: English - Date: 2013-04-10 16:44:55
48Aerodynamics of a Circular Planform Aircraft Bryan Recktenwald1 Auburn University, Alabama, 36832

Aerodynamics of a Circular Planform Aircraft Bryan Recktenwald1 Auburn University, Alabama, 36832

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Source URL: www.eng.auburn.edu

Language: English - Date: 2008-02-25 22:16:24
491  Design and aerodynamic considerations about the civil VTOL aircraft Ray

1 Design and aerodynamic considerations about the civil VTOL aircraft Ray

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Source URL: www.rayaircraft.com

Language: English - Date: 2010-12-16 12:25:47
50RIBLETS FOR TURBULENT DRAG REDUCTION Riblets are low fins approximately aligned with the airflow. Studies at NASA and elsewhere have shown

RIBLETS FOR TURBULENT DRAG REDUCTION Riblets are low fins approximately aligned with the airflow. Studies at NASA and elsewhere have shown

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Source URL: www.ihpva.org

Language: English - Date: 2008-12-22 14:32:59