Essays about: "aerodynamic derivatives"
Showing result 1 - 5 of 8 essays containing the words aerodynamic derivatives.
-
1. Tools and Challenges in Evaluating Control Surface Airworthiness for a Blended-Wing-Body UAV
University essay from KTH/Lättkonstruktioner, marina system, flyg- och rymdteknik, rörelsemekanikAbstract : For transport aeroplanes the Blended-Wing-Body (BWB) configuration shows promise in improving aerodynamic efficiency. The Green Raven project strives to demonstrate hydrogen fuel-cell-electric propulsion on a 4 m wingspan BWB. READ MORE
-
2. Implementation of Flight Mechanical Evaluation Criteria in an Aircraft Conceptual Design Tool with focus on Longitudinal Motions
University essay from Linköpings universitet/Fluida och mekatroniska systemAbstract : This report focuses on the utilisation of flight mechanics in the context of aircraftconceptual design to assess stability, control, and motion characteristics. The pri-mary objective is to acquire the equations of motion and implement longitudinalstability and control criteria using Pacelab Aircraft Preliminary Design 8. READ MORE
-
3. Development of a System Identification Tool for Subscale Flight Testing
University essay from Linköpings universitet/Fluida och mekatroniska systemAbstract : Aircraft system identification has been widely used to this day in applications like control law design, building simulators or extending flight envelopes. It can also be utilized for determining flight-mechanical characteristics in the preliminary design phase of a flight vehicle. READ MORE
-
4. Simulation Model Development of a Subscale Fighter Demonstrator : Aerodynamic Database Generation and Propulsion Modeling
University essay from Linköpings universitet/Fluida och mekatroniska systemAbstract : The main objective of this thesis was to improve the simulation model of a subscale fighter demonstratorthat had been developed previously. In order to give a reliable result, the simulation model should be modeled correctly and employ accurate input. READ MORE
-
5. Uncertainty Analysis of the Aerodynamic Coefficients
University essay from KTH/FlygdynamikAbstract : This thesis treats an error propagation analysis used to estimate the uncertainty of the aerodynamic coefficients. The propagation methods used in this analysis are a Taylor Series Method and a Monte Carlo Method. READ MORE