AERODYNAMICS WING DESIGN UTILITY PROGRAM (A D U P)

• Main Author: Gusti Ngurah Sudira (NIM 23699004), I
• Format: Theses
• Language: Indonesia
• Subjects: Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
• Online Access: https://digilib.itb.ac.id/gdl/view/5094
• Institution: Institut Teknologi Bandung

<b></i>Abstract :</b><i><p align=\"justify\"> <br /> Wing design is a highy complex and important part of the development of an airplane configuration. It is a continually evolving process with a long iteration and supported by many technical discipline. In order to accelerate iteration process, it has to be supported by efficient tool (computer program) which can be operated quickly, user friendly, and independence from big computer (can be operated at the personal computer). <br /> <p align=\"justify\"> <br /> This report explain the result of computer program development which it\'s performance to generate wing geometry and connect it directly to CFD program (VSAERO) through automatically paneling process. The author name this program by Aerodynamics Wing Design Utility Program (ADUP). ADUP is created-based on wing design experienced which is accumulated through wing design procedure. Wing design procedure contains the wing geometry variable which are always iterated in achieving the optimum design. Experience show that most of the time of wing design process had been spended in geometry generation before calculated by CFD program. <br /> <p align=\"justify\"> <br /> In order to shorten wing design process, it has been created ADUP which is concentrated in it\'s performance of wing geometry generation/modification. ADUP was also equipped with data processing of aerodynamics calculation results so that it is easier and quicker to be presented in the picture form. <br />