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REFERENCE LINKING PLATFORM OF KOREA S&T JOURNALS
> Journal Vol & Issue
Journal of the Korean Society for Aviation and Aeronautics
Journal Basic Information
Journal DOI :
The Korean Society for Aviation and Aeronautics
Editor in Chief :
Volume & Issues
Volume 13, Issue 4 - Dec 2005
Volume 13, Issue 3 - Sep 2005
Volume 13, Issue 2 - Jun 2005
Volume 13, Issue 1 - Mar 2005
Selecting the target year
A study on Standards for Pilot Practical Test;Focused on the references for flight training and evaluation
Park, Soo-B ;
Journal of the Korean Society for Aviation and Aeronautics, volume 13, issue 1, 2005, Pages 1~8
The purpose of the study is to show the need for the development of standard materials which can be used for flight training and pilot practical tests in the future. In this paper the flight training and evaluation references of flight training institutes certified by the Ministry of Construction and Transportation(MOCT) are compared with references of the international organization such as ICAO and FAA. As a result it is found that the flight schools certified by the MOCT have used different references for flight training and evaluation. Therefore, this study suggests creation and operation of an expert advisory group to develop new standards for flight training and evaluation, so called " Flight Training Manual", in Korea.
A Study on Aircraft Fuel Requirements
Noh, K.S. ; Choi, Y.C. ; Yoo, K.E. ;
Journal of the Korean Society for Aviation and Aeronautics, volume 13, issue 1, 2005, Pages 9~19
Airplane fuel takes large portion of airline operation cost and recently it has been grown up to about 25% of operating cost. So airlines are making efforts to reduce fuel consumption continuously and also aircraft manufacturers are making efforts to develop less fuel-consuming engines but it takes great expenses and times to develop such engines. In this study, fuel requirements of FAR and JAR, especially contingency fuel requirements, are compared and the effectiveness of each method is analyzed.
Flutter Safety Analysis of a Composite Smart UAV with T-tail Configuration
Kim, D.H. ; Yang, Y.J. ; Jung, S.U. ; Kim, S.J. ; Choi, S.C. ; Kim, S.C. ; Shin, J.W. ;
Journal of the Korean Society for Aviation and Aeronautics, volume 13, issue 1, 2005, Pages 20~31
In this study, subsonic flutter analyses have been conducted for a composite smart UAV with T-tail configuration at the critical flight condition. Detailed three-dimensional finite element model for dynamic analysis is constructed including its nonstructural elements corresponding to installed electronic equipments and fuels. Computational structural dynamics and aeroelastic techniques are conducted using MSC/NASTRAN and originally developed in-house codes. The results for fundamental vibration characteristics and flutter instabilities are presented and compared to each other for different fuel conditions.
Models for Implementation to Aviation Security in Ubiquitus
Kang, J.Y. ; Kim, C.H. ; Jeon, D.K. ;
Journal of the Korean Society for Aviation and Aeronautics, volume 13, issue 1, 2005, Pages 32~42
Concept of ubiquitus computing and networking as a new IT paradigm is introduced and its elementary technologies to implement that philosophy are described. In this paper prioritized models for implementation to the aviation safety in the frame of u-Korea construction are proposed and discussed. Those models are selected in a point of view to embody the ubiquitus society and to satisfy the twin goals of heightened security and increased passenger throughput.
Development of Mold Manufacturing Technology for Small
Jung, D.H. ; Shin, S.K. ; Seong, K.J. ; Song, B.H. ;
Journal of the Korean Society for Aviation and Aeronautics, volume 13, issue 1, 2005, Pages 43~49
There are several ways to mold the complex material, and it is divided to vacuum pack mold, compression mold, and hand lay up for a high molecular substance as a basic material. Moreover, it can be divided to general manufacturing (Single form) and mold manufacturing(Mold form) under normal temperature for Firefly. Firefly was manufactured with hand lay up and general manufacturing that using the foam core, glass fabric, and template without mold. However, mold manufacturing that is producing the surface by semi-sandwich using thin foam core and glass fabric then reinforce the inside with spar and rib is on developing. Mold manufacturing can make easy to production, standardize the quality, and possible to mass producing. In this paper, we present the mold producing process for canard aircraft "Firefly", and the problems and solutions during producing Firefly. Moreover, it complements the defect that the problems caused by master manufacturing error when produce several masters of a large part, and make the manufacturing process to be shortened by the replacement from the supplementary plate to the foam that is installed when producing lay up mold.