Izračun performansi uzlijetanja za zrakoplov Let L-410T

undergraduate thesis

• Title (english): Take-off Performance Calculation for Let L-410T Airplane
• Author: Matej Globlek
• Mentor: Davor Franjković (mentor)
• Committee member: Doris Novak (predsjednik povjerenstva)
• Committee member: Karolina Krajček Nikolić (član povjerenstva)
• Committee member: Anita Domitrović (član povjerenstva)
• Granter: University of Zagreb; Faculty of Transport and Traffic Sciences; (Division of Aeronautics); (Department of Aeronautics); Zagreb
• Defense date and country: 2018-09-17, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Traffic and Transport Technology; Air Traffic

Abstract

Uzlijetanje zrakoplova je dio operacije zrakoplova koji se sastoji od ubrzavanja, uzdizanja nosa zrakoplova, njegova odljepijivanja od USS-e (uzletno-sletna staza) te penjanja do određene visine leta. Poslije slijetanja najkritičniji je dio leta. Za bilo koje uzlijetanje najvažnije je pokazati da potrebna duljina za uzlijetanje ne prekoračuje raspoloživu duljinu za uzlijetanje aerodroma. U ovom završnom radu će se govoriti o performansama uzlijetanja zrakoplova Let L-410T, odnosno o njihovom izračunu. Performanse uzlijetanja ovise o nizu čimbenika: masi uzlijetanja zrakoplova i njegovu težištu, temperaturi, gustoći zraka, vjetru, površini i nagibu USS-e, položaju zakrilaca te kontaminaciji zrakoplovne strukture. Utjecaji ovih čimbenika na zrakoplov Let L-410T, odnosno na njegovu potrebnu duljinu za uzlijetanje, brzine uzlijetanja i pilotske procedure za uz1ijetanje, bit će detaljnije objašnjeni u radu.

Abstract (english)

Aircraft take-off is the part of aircraft operation which consists of acceleration, raising the nose of aircraft, lifting off the runway and climbing to the certain altitude. After landing, it is the most critical phase of flight. For any particular take-off it must be shown that required take-off distance does not exceed the take-off distance available at the aerodrome. In this final work it will be talked about take-off performance of the airplane Let L-410T, respectively about their calculation. Take-off performance depends on many factors: aircraft take-off mass and aircraft center of gravity, temperature, air density, wind, runway surface and runway slope, flap setting and airframe contamination. Effects of these factors on airplane Let L-410T, respectively on its required take-off distance, take-off speeds and pilot take-off procedures, will be explained more indepth in the work.

• Keywords: zrakoplov Let L-410T-; tehničke karakteristike zrakoplova; uzlijetanje; performanse uzlijetanja
• Keywords (english): airplane Let L-410T; airplane specifications; take-off; take-off performance
• Language: croatian
• URN:NBN: urn:nbn:hr:119:803463
• Study programme: Title: Aeronautics; Study programme type: university; Study level: undergraduate; Academic / professional title: sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike (sveučilišni/a prvostupnik/prvostupnica (baccalaureus/baccalaurea) inženjer/inženjerka aeronautike)
• Type of resource: Text
• File origin: Born digital
• Access conditions: Open access
• Created on: 2018-10-29 12:28:06