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[PDF] Aircraft Engine Design (AIAA Education Series) Read Online. 5, 30 April 2012 | AIAA Journal, Vol. . 1, © 2021 American Institute of Aeronautics and Astronautics, American Institute of Aeronautics and Astronautics, Journal of Guidance, Control, and Dynamics, Journal of Thermophysics and Heat Transfer, Airplane Design Optimization for Minimal Global Warming Impact, Device for Contact Measurement of Turbine Blade Geometry in Robotic Grinding Process, Enhanced cruise range prediction for narrow-body turbofan commercial aircraft based on QAR data, The design and validation of over/under turbine-based combined cycle inlet, Computational Modelling and Analysis of Porous Bleed Holes at Supersonic Speeds, Distortion Elimination for Serpentine Inlet Using CoFlow Jet Flow Control with Variation of Mach Numbers, Conceptual design of small aircraft with hybrid-electric propulsion systems, Prediction of compressor nominal characteristics of a turboprop engine using artificial neural networks for build standard assessment, Design Tools for Conceptual Analysis of Future Commercial Supersonic Aircraft, Tail Sizing Considerations for Wingtip Propulsor Driven Aircraft Applied to the Parallel Electric-Gas Architecture with Synergistic Utilization Scheme (PEGASUS) Concept, Differential Dynamic Programming to Critical-Engine-Inoperative Takeoff Certification Analysis, Mitigation of Serpentine Duct Flow Distortion Using CoFlow Jet Active Flow Control, Global Aero-Structural Design Optimization of More Flexible Wings for Commercial Aircraft, Sizing of a Turboprop Engine Powered High Altitude Unmanned Aerial Vehicle and It`s Propulsion System for an Assumed Mission Profile in Turkey, Development and application of a preliminary design methodology for modern low emissions aero combustors, Status and Characteristics of Unmanned Aerial Vehicle Gas Turbine Engines, Initial Sizing Methodology for Hybrid-Electric General Aviation Aircraft, New Adaptive Algorithm Development for Monitoring Aircraft Performance and Improving Flight Management System Predictions, Thermodynamic design and optimization of the multi-branch closed Brayton cycle based precooling-compression system for a novel hypersonic aeroengine, Analysis and Prevention of Snags in Turboshaft Engines During Calibration Test, Flow Characterization and Combustion Analysis for a Disk-Oriented Engine, A Comparison of Hybrid-Electric Aircraft Sizing Methods, Tradespace Exploration and Analysis Using Mission Effectiveness in Aircraft Conceptual Design, High fidelity simulations of supersonic intakes, Erweiterung des Betriebsbereiches durch Stabilisierungsmaßnahmen, Aerodynamic optimization of propellers for High Altitude Pseudo-Satellites, SIZING OF A TURBOPROP ENGINE POWERED HIGH ALTITUDE UNMANNED AERIAL VEHICLE AND IT`S PROPULSION SYSTEM FOR AN ASSUMED MISSION PROFILE IN TURKEY, Control-oriented low-speed dynamic modeling and trade-off analysis of air-breathing aerospace vehicles, Comparison of model predictive controller and optimized min-max algorithm for turbofan engine fuel control, Performance analysis of aircraft fuel tank inerting system with turbocharger, Analysis and Prevention of Failures in a Turboprop Engine, Computational fluid dynamics-based approach for low-order models of propelling nozzle performance, Dominant Suborbital Space Tourism Architectures, Impact of electric propulsion technology and mission requirements on the performance of VTOL UAVs, Design and implementation of MPC for turbofan engine control system, Thermodynamic analysis of the influential mechanism of fuel properties on the performance of an indirect precooled hypersonic airbreathing engine and vehicle, An Analysis of the Strayton Engine, a Brayton and Stirling Cycle Recuperating Engine, A Medial-Object-based Design-in-Context Approach for the Structural Design of Engine Subsystems, Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system, Investigation of Loss Reduction in a High Lift Turbine by Localized Endwall Jets, Identification and Validation of an Engine Performance Database Model for the Flight Management System, Overall optimization design of high temperature components cooling coefficient for lower infrared turbofan engine, A Design Method of Steady State Control Law for Civil Turbofan Engine, Integrated Sizing and Optimization of Hybrid Wing Body Aircraft in Conceptual Design, Modeling of a Modern Aircraft Through Calibration Techniques, Adaptation of General Aviation Techniques for the Design of a Supersonic Leading-Edge Business Jet, Multi-mission Multi-objective Optimization in Commercial Aircraft Conceptual Design, Computational study of characteristics of intake flow in model axial compressor with regard to different variants of “active disk” boundary condition, Failure Analysis of a Cam Gear in the Torquemeter Assembly of a Turboprop Engine, Cessna Citation X simulation turbofan modelling: identification and identified model validation using simulated flight tests, Turbofan engine performance optimization based on aircraft cruise thrust level, Jet engine degradation prognostic using artificial neural networks, Experimental Investigation of Flow Characteristics in an Ultra Compact Combustor, Interference Drag Associated with Engine Locations for Multidisciplinary Design Optimization, New Algorithm for Fuel Flow Prediction and its Correction during the Cruise - Application on the Cessna Citation X Business Aircraft, MBSE-enabled Interactive Environment for Aircraft Conceptual Sizing & Synthesis, Model-Based Approach to the Requirements Analysis for a Conceptual Aircraft Sizing and Synthesis Problem, Conceptual design of a fifth generation unmanned strike fighter, Analytical Modelling and Validation of a Turbofan Engine at Design Conditions, Comparison of Electric Ducted Fans for Future Green Aircrafts, On Aircraft Design Under the Consideration of Hybrid-Electric 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