Cöllen, Liana, Rizzi, Arthur and Gollnick, Volker (2011) Standardized Geometry Formats for Aircraft Conceptual Design and Physics-based Aerodynamics and Structural Analyses. Royal Institute of Technology (KTH) Aeronautical and Vehicle Engineering Aerodynamics, Stockholm.
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4.1 Airbus A320 ( PDFDrive ).pdf - Published Version Download (5MB) |
Abstract
Present trends in aircraft design towards configurations with augmented stability or operations in expanded flight envelopes require accurate predictions of the flight-dynamic behavior. The process of aircraft design is split up into three phases depicted in figure1.1. In the conceptual design phase the configuration arrangement, size, weight, and performance of the aircraft are defined by fulfilling requirements of the customer. Hence, conceptual design is a fluid process where new ideas and problems occur. During the preliminary design phase specialists in the areas of structure, landing gear, and control systems design and analyze the components of the aircraft. Preliminary design has to establish confidence to build the aircraft on time with the estimated costs. In the detail design phase the precise geometry of the components are designed for fabrication considering producibility. Besides accomplishing structure test flights, control systems are simulated and tested by pilots. After successful completion of the three phases in aircraft design the aircraft will be manufactured [12]. Conceptual design is the primary focus of this research project.
| Item Type: | Book |
|---|---|
| Subjects: | H Social Sciences > HE Transportation and Communications Q Science > QC Physics T Technology > TA Engineering (General). Civil engineering (General) T Technology > TL Motor vehicles. Aeronautics. Astronautics |
| Divisions: | Politeknik Penerbangan |
| Depositing User: | Ms PKL 2 S1 Unair |
| Date Deposited: | 25 Feb 2022 08:09 |
| Last Modified: | 25 Feb 2022 08:09 |
| URI: | http://repo.poltekbangsby.ac.id/id/eprint/628 |
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