MODEL BASED OPTIMIZATION OF PROPULSION INVERTER FOR MORE-ELECTRIC AIRCRAFT APPLICATIONS USING DOUBLE FOURIER INTEGRAL ANALYSIS

MODEL BASED OPTIMIZATION OF PROPULSION INVERTER FOR MORE-ELECTRIC AIRCRAFT APPLICATIONS USING DOUBLE FOURIER INTEGRAL ANALYSIS

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:AIAA Propulsion and Energy Forum (2020 : Online) Electric aircraft technologies
1. Verfasser: Hassan, Mustafeez U. (VerfasserIn)
Weitere Verfasser: Yuan, Zhao (VerfasserIn), Peng, Hongwu (VerfasserIn), Emon, Asif Imran (VerfasserIn), Chen, Yingzhuo (VerfasserIn), Luo, Fang (VerfasserIn)
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2020
Schlagworte:
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Titel Jahr Verfasser
ELECTROMAGNETIC ANALYSIS OF FULLY SUPERCONDUCTING SYNCHRONOUS MACHINES FOR FUTURE TURBO ELECTRIC PROPULSION SYSTEMS 2020 Terao, Yutaka
DEVELOPMENT OF POWER DENSE SUPERCONDUCTING DC NETWORKS FOR ELECTRIC AIRCRAFT 2020 Cheetham, Peter
PARALLEL HYBRID PROPULSION & SECONDARY POWER SYSTEM ARCHITECTURE EXPLORATION AND EVALUATION 2020 Lents, Charles E.
NASA ELECTRIC AIRCRAFT TESTBED (NEAT) RECONFIGURATION TO ENABLE ALTITUDE TESTING OF MEGAWATT-SCALE MOTOR 2020 Haglage, Joe
OUTER STATOR MAGNETICALLY GEARED MOTORS FOR ELECTRIFIED URBAN AIR MOBILITY VEHICLES 2020 Tallerico, Thomas
PUTTING UNIVERSITIES IN CHARGE YIELDS EARLY SUCCESS FOR NASA AERONAUTICS 2020 Datta, Koushik
OUTER MOLD LINE COOLED ELECTRIC MOTORS FOR ELECTRIC AIRCRAFT 2020 Tallerico, Thomas
POWER DISTRIBUTION AND THERMAL MANAGEMENT MODELING FOR ELECTRIFIED AIRCRAFT 2020 Byahut, Saakar
DESIGN OF ELECTRIC MACHINE FOR ELECTRIC AIRCRAFT: A CASE STUDY OF ROTOR-STATOR CONFIGURATIONS AND MAGNET ARRANGEMENTS 2020 Mitsuda, Hiroshi
CONCEPTUAL DESIGN AND OPERATING COSTS EVALUATION OF A 19-SEAT ALL- ELECTRIC AIRCRAFT FOR REGIONAL AVIATION 2020 Monjon, Matheus M.
HIGH-EFFICIENCY TURBOELECTRIC PROPULSION DRIVE BASED ON MEDIUM- VOLTAGE SIC INDIRECT MATRIX CONVERTER 2020 Luckett, Ben
ANALYTICAL MODEL AND DESIGN SPACE STUDIES A SUPERCONDUCTING MACHINE FOR AN AIRCRAFT APPLICATION 2020 Tangudu, Jagadeesh
MULTI-POINT DESIGN OF PARALLEL HYBRID AERO ENGINES 2020 Sielemann, Michael
INTEGRATED PROPULSIVE AND THERMAL MANAGEMENT SYSTEM DESIGN FOR OPTIMAL HYBRID ELECTRIC AIRCRAFT PERFORMANCE 2020 Abolmoali, Philip C.
CO-DESIGN OF AN INTEGRATED DIRECT-DRIVE ELECTRIC MOTOR AND PROPELLER FOR AIRCRAFT PROPULSION 2020 Balachandran, Thanatheepan
DESCENT ANGLE CONTROL BY REGENERATIVE AIR BRAKE USING OBSERVER- BASED THRUST CONTROL FOR ELECTRIC AIRCRAFT 2020 Yokota, Kentaro
BATTERY EVALUATION PROFILES FOR X-57 AND FUTURE URBAN ELECTRIC AIRCRAFT 2020 Chin, Jeff
WIRELESS POWER TRANSFER WITH TEMPERATURE MONITORING INTERFACE FOR HELICOPTER ROTOR BLADE ICE PROTECTION 2020 Brunetti, Massimo
ANALYSIS OF SELF-COOLING METHOD OF A ROTOR USING BUOYANCY DRIVEN CONVECTION 2020 Kabir, Rifat
COMPUTATIONAL EVALUATION OF AN OML-BASED HEAT EXCHANGER CONCEPT FOR HEATHER 2020 Sozer, Emre
Alle Artikel auflisten