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Wingbox
Stress Analysis of an Aircraft Fuselage with and Without Portholes Using
For Improved Airplane Performance
Aviation Week & Space Technology
Sizing and Layout Design of an Aeroelastic Wingbox Through Nested Optimization
Structural Analysis of a Wing Box
Tailored Wingbox Structures Through Additive Manufacturing: a Summary of Ongoing Research at NASA Larc
Department of the Air Force
Qtr 02 09 a Quarterly Publication Boeing.Com/Commercial/ Aeromagazine
Systems Study for an Integrated Digital/Electric Aircraft (IDEA)
Design and Development of a Multi- Mission UAS Through Modular Component Integration and Additive Manufacturing
Structural Certification of the F-16 Block 52+ Aircraft 29 November 2005 2005 USAF Aircraft Structural Integrity Program Conference
Cessna 525A Citation CJ2+, N380CR No & Type of Engines
Landing Gear Design in an Automated Design Environment
In-Flight Wingtip Folding: Inspiration from the XB-70 Valkyrie Gaétan X
Structural Wingbox Optimization in a Coupled FSI Problem of a Flexible Wing: FEA Sol200 Versus Surrogate Models Joseph Morlier, M
Design of an Innovative Wing Tip Device
In-Flight Wingtip Folding: Inspiration from the XB-70 Valkyrie
04 by Providing More Capacity Than Any Other Twin-Engine Freighter, the 777F Brings New Levels of Efficiency to the Long-Haul M
Top View
Lightweight Structures in Technical Engineering
Airframe Wingbox Preliminary Design and Weight Prediction
Conceptual Design of Civil Airplane Composite Wingbox Structures
Design and Structural Optimization of a Flying Wing of Low Aspect Ratio Based on Flight Loads
Knowledge-Based Engineering Approach to the Finite Element Analysis of Fuselage Structures
A Framework for Unconventional Landing Gear Configuration Modelling
STINGRAEIsOnTheOrderOf30%MoreFuelEfficientThanTheBoeing737 800. 2
Stress Analysis and Weight Optimization of a Wing Box Structure Subjected to Flight Loads
A Certification-Driven Platform for Multidisciplinary Design Space
Electroimpact Projects
Investigating the Benefits of Morphing Wing Tip Devices - a Case Study
HALE Multidisciplinary Design Optimization Part I: Solar-Powered Single and Multiple-Boom Aircraft
Full-Scale Drop Test of a Fokker F28 Wingbox Fuselage Section J. D. Littell1
Commercial Transport Aircraft Composite Wing Box Trade Study
Structural Design and Modelling of the Zigzag Wingbox for Span Morphing Wing
Multidisciplinary Design Optimisation for Aircraft Wing Mass Estimation
Cranfield University James E Gautrey Flying Qualities
Aerodynamic and Structural Design of a Winglet for Enhanced Performance of a Business Jet