Open Access. Powered by Scholars. Published by Universities.®
Systems Engineering and Multidisciplinary Design Optimization Commons™
Open Access. Powered by Scholars. Published by Universities.®
- Discipline
-
- Space Vehicles (21)
- Aeronautical Vehicles (19)
- Aviation (19)
- Navigation, Guidance, Control and Dynamics (14)
- Aviation Safety and Security (12)
-
- Aerodynamics and Fluid Mechanics (11)
- Operations Research, Systems Engineering and Industrial Engineering (11)
- Propulsion and Power (11)
- Physical Sciences and Mathematics (10)
- Social and Behavioral Sciences (10)
- Multi-Vehicle Systems and Air Traffic Control (9)
- Other Aerospace Engineering (9)
- Computer Engineering (8)
- Computer Sciences (7)
- Electrical and Computer Engineering (7)
- Structures and Materials (7)
- Management and Operations (6)
- Systems Engineering (6)
- Artificial Intelligence and Robotics (5)
- Astrodynamics (5)
- Aviation and Space Education (5)
- Education (5)
- Space Habitation and Life Support (5)
- Psychology (4)
- Risk Analysis (4)
- Robotics (4)
- Business (3)
- Keyword
-
- Advanced Air Mobility (3)
- Antenna arrays (2)
- Aviation (2)
- Blades (2)
- CFD (2)
-
- Design (2)
- Electronic Flight Bag (2)
- Genetic algorithms (2)
- Hypersonics (2)
- NextGen (2)
- Propulsion (2)
- Reinforcement Learning (2)
- Unmanned aircraft systems (2)
- 36-rotor multicopter (1)
- AI certification (1)
- AI integration in safety-critical systems (1)
- AI safety assurance (1)
- AI-enabled computer-based control system / AI-CBCS (1)
- Abrasion (1)
- Adaptive arrays (1)
- Adaptive control (1)
- Advanced Air Mobility (AAM) (1)
- Advanced Air Mobility (AAM); Urban Air Mobility (UAM); electric vertical takeoff and landing aircraft (eVTOL); air taxi routing; aircraft noise; noise-aware route optimization; trajectory optimization; multi-objective optimization; vertiport network design; geographic information systems (GIS); air transportation simulation (1)
- Advanced aerial mobility (1)
- Aero-GNC coupling (1)
- Aerodynamic identification (1)
- Aeroelastic (1)
- Aeronautical Engineering (1)
- Aerospace (1)
- Aerospace Technology. Public Acceptance (1)
- Publication Year
- Publication
-
- International Journal of Aviation, Aeronautics, and Aerospace (24)
- Discovery Day - Daytona Beach (18)
- Doctoral Dissertations and Master's Theses (14)
- Publications (12)
- Master's Theses - Daytona Beach (7)
-
- Space Traffic Management Conference (4)
- Discovery Day - Prescott (2)
- Journal of Aviation/Aerospace Education & Research (2)
- National Training Aircraft Symposium (NTAS) (2)
- Student Research Symposium (SRS) (2)
- Student Works (2)
- Aviation / Aeronautics / Aerospace International Research Conference (1)
- Beyond: Undergraduate Research Journal (1)
- ERAU Prescott Aviation History Program (1)
- Human Factors and Applied Psychology Student Conference (1)
- Undergraduate Student Works (1)
- Publication Type
Articles 91 - 94 of 94
Full-Text Articles in Systems Engineering and Multidisciplinary Design Optimization
An Intermittent-Combustion General Aviation Aircraft Engine Exhaust Noise Prediction Algorithm, Hiroko Tada
An Intermittent-Combustion General Aviation Aircraft Engine Exhaust Noise Prediction Algorithm, Hiroko Tada
Master's Theses - Daytona Beach
From an environmental point of view, the reduction of aircraft noise has become an important factor recently. There are two factors that make airplane noise: propeller noise and engine noise. This report puts emphasis on only the engine noise in order to begin understanding what airplane engine exhaust noise is. At first, the engine exhaust noise is comprehended using the Dobrzynski's engine noise theory. Next, a discussion about an Embry-Riddle Aeronautical University (ERAU) engine system, engine exhaust system configurations, and microphone setting standards that show the ERAU engine system exhaust noise data. Finally, an Intermittent-Combustion (IC) General Aviation (GA) aircraft …
A Comparison Of Pseudo 3-Dimensional Collision Avoidance-Predictor Displays For Free Flight, Steve Kertesz Jr.
A Comparison Of Pseudo 3-Dimensional Collision Avoidance-Predictor Displays For Free Flight, Steve Kertesz Jr.
Master's Theses - Daytona Beach
This study was the second of two studies to evaluate the use of a pseudo three-dimensional display to present information about future possible conflicts. The purpose of this study was to evaluate variations of a cockpit screen display that transfers relevant data to the pilot in a manner which is easy to interpret and to facilitate the possible stressful situations that may be encountered due to the proposed free flight environment. In the first phase, three display concepts, using three different screen designs were compared. In this study, three different displays, all of which used using the space-time predictor concept …
Dynamic Simulation Of General Aviation Cabin Environments And Occupant Restraint Systems, Mark A. Shilladay
Dynamic Simulation Of General Aviation Cabin Environments And Occupant Restraint Systems, Mark A. Shilladay
Master's Theses - Daytona Beach
After a five year study of General Aviation (GA) accidents, the National Transportation Safety Board (NTSB) has concluded that aircraft cabin environments place the occupant at high risk of suffering severe injuries in an emergency crash situation. Studies of Federal Aviation Administration (FAA) seat tests were used to form the basis of a computer analysis to address dynamic cabin environments. In this effort a simplified system of masses, springs, and dampers are used to simulate the more complex configuration of cabin structure, seat, pilot, and restraints on a personal computer. The primary objective of this study is to accurately simulate …
Optimized Engine Out Procedures To Extend The Range Of Jet Transport Airplanes, Miltos Miltiadous
Optimized Engine Out Procedures To Extend The Range Of Jet Transport Airplanes, Miltos Miltiadous
Master's Theses - Daytona Beach
The purpose of this study was to develop optimum engine-out procedures for the Boeing 747 and 767 on extended flights that will increase the range of the aircraft in case of engine failure. Theory suggests that an optimum amount of bank angle that will minimize drag resulting from asymmetric thrust in a multiengine airplane experiencing an engine failure, can be determined. By banking the airplane into the operative engines by that optimum bank angle, the range of the airplane can be improved significantly. Wind tunnel tests of both a Boeing 747 and a 767 model were performed to determine experimentally …