ANALISIS PRESTASI MENANJAK (CLIMB PERFORMANCE) PADA UJI TERBANG PESAWAT UDARA
<b></i>Abstract :</b><i><p align=\"justify\"> <br /> The climb performance of an aircraft is an important safety of flight consideration as it determines the capability of the aircraft to clear an obstacle after take off in the take off configuration. D...
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id-itb.:51272006-06-06T13:12:00ZANALISIS PRESTASI MENANJAK (CLIMB PERFORMANCE) PADA UJI TERBANG PESAWAT UDARA Hakiem , Nashrul Teknik (Rekayasa, enjinering dan kegiatan berkaitan) Indonesia Theses Flight test, climb performance, rate of climb INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/5127 <b></i>Abstract :</b><i><p align=\"justify\"> <br /> The climb performance of an aircraft is an important safety of flight consideration as it determines the capability of the aircraft to clear an obstacle after take off in the take off configuration. Due to the safety of flight considerations the F.A.A. has minimum rate of climb and climb gradient (angle of climb) criteria for those flight modes close to the ground such as take-off and landing. <br /> In this thesis, a software to analysis climb performance of a turboprop aircraft with sawtooth climb has been developed. This software is called ClimPerf. The data parameter of the ClimPerf software is received from real time System 500. <br /> Development of the ClimPerf software uses waterfall methodology. The design of the software is implemented on the personal computer having windows 98 operating system, using Visual Basic 6.0 programming language. <br /> text |
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Teknik (Rekayasa, enjinering dan kegiatan berkaitan) Hakiem , Nashrul ANALISIS PRESTASI MENANJAK (CLIMB PERFORMANCE) PADA UJI TERBANG PESAWAT UDARA |
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<b></i>Abstract :</b><i><p align=\"justify\"> <br />
The climb performance of an aircraft is an important safety of flight consideration as it determines the capability of the aircraft to clear an obstacle after take off in the take off configuration. Due to the safety of flight considerations the F.A.A. has minimum rate of climb and climb gradient (angle of climb) criteria for those flight modes close to the ground such as take-off and landing. <br />
In this thesis, a software to analysis climb performance of a turboprop aircraft with sawtooth climb has been developed. This software is called ClimPerf. The data parameter of the ClimPerf software is received from real time System 500. <br />
Development of the ClimPerf software uses waterfall methodology. The design of the software is implemented on the personal computer having windows 98 operating system, using Visual Basic 6.0 programming language. <br />
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Theses |
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Hakiem , Nashrul |
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Hakiem , Nashrul |
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Hakiem , Nashrul |
title |
ANALISIS PRESTASI MENANJAK (CLIMB PERFORMANCE) PADA UJI TERBANG PESAWAT UDARA |
title_short |
ANALISIS PRESTASI MENANJAK (CLIMB PERFORMANCE) PADA UJI TERBANG PESAWAT UDARA |
title_full |
ANALISIS PRESTASI MENANJAK (CLIMB PERFORMANCE) PADA UJI TERBANG PESAWAT UDARA |
title_fullStr |
ANALISIS PRESTASI MENANJAK (CLIMB PERFORMANCE) PADA UJI TERBANG PESAWAT UDARA |
title_full_unstemmed |
ANALISIS PRESTASI MENANJAK (CLIMB PERFORMANCE) PADA UJI TERBANG PESAWAT UDARA |
title_sort |
analisis prestasi menanjak (climb performance) pada uji terbang pesawat udara |
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https://digilib.itb.ac.id/gdl/view/5127 |
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