#TITLE_ALTERNATIVE#

This final project contains of a method (step integration method) to calculate takeoff field length of Boeing 737-400 based on simple theoretical equations. The results of this method are compared with the operation manual of Boeing 737-400. Inputs of flight condition such as runway altitude, flap p...

Full description

Saved in:
Bibliographic Details
Main Author: IQBAL ZULHAJRI (NIM 13602015); Pembimbing : Dr. Ir. Toto Indriyanto, MUHAMMAD
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/16574
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:16574
spelling id-itb.:165742017-10-09T10:33:28Z#TITLE_ALTERNATIVE# IQBAL ZULHAJRI (NIM 13602015); Pembimbing : Dr. Ir. Toto Indriyanto, MUHAMMAD Indonesia Final Project INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/16574 This final project contains of a method (step integration method) to calculate takeoff field length of Boeing 737-400 based on simple theoretical equations. The results of this method are compared with the operation manual of Boeing 737-400. Inputs of flight condition such as runway altitude, flap position, wind speed and runway slope are also evaluated to see wether the method in calculating takeoff field length can give closer results to the operation manual. Then, conclusion is taken from analysis and calculation in this final project that step integration method can be refered as a method to analyse takeoff field length of other type of airplane. 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 This final project contains of a method (step integration method) to calculate takeoff field length of Boeing 737-400 based on simple theoretical equations. The results of this method are compared with the operation manual of Boeing 737-400. Inputs of flight condition such as runway altitude, flap position, wind speed and runway slope are also evaluated to see wether the method in calculating takeoff field length can give closer results to the operation manual. Then, conclusion is taken from analysis and calculation in this final project that step integration method can be refered as a method to analyse takeoff field length of other type of airplane.
format Final Project
author IQBAL ZULHAJRI (NIM 13602015); Pembimbing : Dr. Ir. Toto Indriyanto, MUHAMMAD
spellingShingle IQBAL ZULHAJRI (NIM 13602015); Pembimbing : Dr. Ir. Toto Indriyanto, MUHAMMAD
#TITLE_ALTERNATIVE#
author_facet IQBAL ZULHAJRI (NIM 13602015); Pembimbing : Dr. Ir. Toto Indriyanto, MUHAMMAD
author_sort IQBAL ZULHAJRI (NIM 13602015); Pembimbing : Dr. Ir. Toto Indriyanto, MUHAMMAD
title #TITLE_ALTERNATIVE#
title_short #TITLE_ALTERNATIVE#
title_full #TITLE_ALTERNATIVE#
title_fullStr #TITLE_ALTERNATIVE#
title_full_unstemmed #TITLE_ALTERNATIVE#
title_sort #title_alternative#
url https://digilib.itb.ac.id/gdl/view/16574
_version_ 1820745409875673088