DEVELOPMENT OF CALCULATION METHOD TO OBTAIN AERODYNAMIC STABILITY DERIVATIVES OF B747-200 AIRCRAFT IN X-PLANE SIMULATOR

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Bibliographic Details
Main Author: ROZAK FASSAH, ABDUL
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/52839
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:52839
spelling id-itb.:528392021-02-22T00:00:00ZDEVELOPMENT OF CALCULATION METHOD TO OBTAIN AERODYNAMIC STABILITY DERIVATIVES OF B747-200 AIRCRAFT IN X-PLANE SIMULATOR ROZAK FASSAH, ABDUL Indonesia Final Project INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/52839 text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description
format Final Project
author ROZAK FASSAH, ABDUL
spellingShingle ROZAK FASSAH, ABDUL
DEVELOPMENT OF CALCULATION METHOD TO OBTAIN AERODYNAMIC STABILITY DERIVATIVES OF B747-200 AIRCRAFT IN X-PLANE SIMULATOR
author_facet ROZAK FASSAH, ABDUL
author_sort ROZAK FASSAH, ABDUL
title DEVELOPMENT OF CALCULATION METHOD TO OBTAIN AERODYNAMIC STABILITY DERIVATIVES OF B747-200 AIRCRAFT IN X-PLANE SIMULATOR
title_short DEVELOPMENT OF CALCULATION METHOD TO OBTAIN AERODYNAMIC STABILITY DERIVATIVES OF B747-200 AIRCRAFT IN X-PLANE SIMULATOR
title_full DEVELOPMENT OF CALCULATION METHOD TO OBTAIN AERODYNAMIC STABILITY DERIVATIVES OF B747-200 AIRCRAFT IN X-PLANE SIMULATOR
title_fullStr DEVELOPMENT OF CALCULATION METHOD TO OBTAIN AERODYNAMIC STABILITY DERIVATIVES OF B747-200 AIRCRAFT IN X-PLANE SIMULATOR
title_full_unstemmed DEVELOPMENT OF CALCULATION METHOD TO OBTAIN AERODYNAMIC STABILITY DERIVATIVES OF B747-200 AIRCRAFT IN X-PLANE SIMULATOR
title_sort development of calculation method to obtain aerodynamic stability derivatives of b747-200 aircraft in x-plane simulator
url https://digilib.itb.ac.id/gdl/view/52839
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