Utjecaj mase jednomotornog klipnog zrakoplova na performanse u režimu penjanja

undergraduate thesis

• Title (english): Influence of a Single-engine Piston Aircraft Mass on Climb Performance
• Author: Ivan Vitek
• Mentor: Petar Andraši (mentor)
• Committee member: Doris Novak (predsjednik povjerenstva)
• Committee member: Karolina Krajček Nikolić (član povjerenstva)
• Committee member: Davor Franjković (član povjerenstva)
• Granter: University of Zagreb; Faculty of Transport and Traffic Sciences; (Division of Aeronautics); (Department of Aeronautics); Zagreb
• Defense date and country: 2020-09-15, Croatia
• Scientific / art field, discipline and subdiscipline: TECHNICAL SCIENCES; Traffic and Transport Technology; Air Traffic

Abstract

Performanse predstavljaju specifičnu skupinu sposobnosti koju određeni zrakoplov posjeduje u rasponu različitih masa i brzina na određenim visinama i u određenim fazama leta (horizontalni let, penjanje, spuštanje, polijetanje, slijetanje i zaokreti). Ovaj rad analizira performanse u režimu penjanja. Eksperiment je izveden u tri leta sa penjanjem do visine 8000 stopa gdje su mjereni podaci o brzini uzdizanja, temperaturi, vremenu penjanja, potrošenom gorivu i prijeđenoj udaljenosti. Rezultati mjerenja prikazani su tablično. Kroz analizu rezultata, objašnjeni su i bitni vanjski čimbenici koji se moraju uzeti u obzir pri cjelokupnom izračunu performansi.

Abstract (english)

Performance represents a specific group of capabilities that a particular aircraft possesses in a range of different masses and speeds at certain altitudes and at certain stages of flight (horizontal flight, climb, descent, take-off, landing and turns). This paper analyzes the performance in climbing regime. The experiment was performed in three flights with climbing to an altitude of 8000 feet where data on climb speed, climbing time, temperature, fuel consumption and distance traveled were measured. The measurement results are shown in the tables. Through the analysis of the results, the important external factors that must be taken into account in the overall performance calculation are also explained.

• Keywords: performanse zrakoplova; režim penjanja; rezultati eksperimenta; masa zrakoplova
• Keywords (english): aircraft performance; climb regime; experimental results; aircraft mass
• Language: croatian
• URN:NBN: urn:nbn:hr:119:841355
• 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: 2020-10-23 11:09:51