STRUCTURAL ANALYSIS OF AN EQUIVALENT BOX-WING REPRESENTATION OF SENSORCRAFT JOINED-WING CONFIGURATION FOR HIGH-ALTITUDE, LONG-ENDURANCE (HALE) AIRCRAFT
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- Type
- article
- Published
- 2005-07-13
- Cited by
- 7
- References
- 24
- Access
- Open access
- OpenAlex
- https://openalex.org/W153824
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:107456121
Keywords
Wing, Wing configuration, Representation (politics), Aeronautics, Engineering
References
- Preliminary design optimization of joined-wing aircraft
- Structural Weight Comparison of a Joined Wing and a Conventional Wing
- Joined-Wing Aeroelastic Design with Geometric Nonlinearity
- The joined wing - An overview
- Parametric weight evaluation of joined wings by structural optimization
- Joined-wing research airplane feasibility study
- The design of a joined wing flight demonstrator aircraft
- Aerodynamic and structural studies of joined-wing aircraft
- Structurally Integrated Antennas on a Joined-Wing Aircraft
- Structural optimization for joined-wing synthesis
- Application of Active-Aeroelastic-Wing Technology to a Joined-Wing Sensorcraft
- Influence of joint fixity on the aeroelastic characteristics of a joined wing structure
- Aeroelasticity of joined-wing airplane configurations - Past work and future challenges - a survey
- PREDICTION OF STRUCTURAL BEHAVIOR OF JOINED-WING CONFIGURATION OF HIGH-ALTITUDE LONG-ENDURANCE (HALE) AIRCRAFT *
- AERODYNAMIC ANALYSIS OF THE JOINED-WING CONFIGURATION OF A HIGH-ALTITUDE, LONG ENDURANCE (HALE) AIRCRAFT
- STRUCTURAL ANALYSIS OF REINFORCED SHELL WING MODEL FOR JOINED-WING CONFIGURATION
- Aeroelastic Analysis Of Joined Wing Of High Altitude Long Endurance (HALE) Aircraft Based On The Sensor-Craft Configuration
- Finite Element Procedures
Cited by
- Multi-Objective and Multidisciplinary Design Optimisation (MDO) of UAV Systems using Hierarchical Asynchronous Parallel Evolutionary Algorithms
- Multi-Objective and Multidisciplinary Design Optimisation of Unmanned Aerial Vehicle Systems using Hierarchical Asynchronous Parallel Multi-Objective Evolutionary Algorithms
- Experiments with Geometric Non-Linear Coupling for Analytical Validation
- Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future
- Experiments with Geometric Nonlinear Coupling for Analytical Validation
- FOLLOWER FORCE EXPERIMENTS WITH GEOMETRIC NON-LINEAR COUPLING FOR ANALYTICAL VALIDATION THESIS
- Follower-Force Experiments with Geometric Non-Linear Coupling for Analytical Validation
- Follower-Force Experiments with Geometric Non-Linear Coupling for Analytical Validation
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