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Publications by Thomas Klimmek
Design and Sizing of an Aeroelastic Composite Model for a Flying Wing Configuration With Maneuver, Gust, and Landing Loads
CEAS Aeronautical Journal
Transportation
Aerospace Engineering
Aero-Structural Optimization of the NASA Common Research Model
Related publications
Nonlinear Aeroelastic Response of Highly Flexible Flying Wing Due to Different Gust Loads
Robust Structural Design for Active Aeroelastic Wing With Aerodynamic Uncertainties
Aeroelastic Stability and Performance Characteristics of Aircraft With Advanced Composite Sweptforward Wing Structures
Aerodynamic Design Considerations of a Flying Wing Type Uav
SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE
Nonlinear Aeroelastic Modeling of a Flexible Wing and Comparison With Experiments
Rolling Active Control for an Aircraft of Seamless Aeroelastic Wing
Mars Entry, Descent, and Landing Parametric Sizing and Design Space Visualization Trades
Uav Flying Wing With a Photovoltaic System
Review of the Air Force Academy
High Lift Design and Aerodynamic Assessment for an Over-The-Wing Pylon-Mounted Engines Configuration With STOL Capabilities
